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+design_id,animals,traits,animal_count,trait_count,empty_mass_kg,payload_mass_kg,rotor_count,max_twr,burst_power_factor,burst_duration_s,unsteady_lift_gain,energy_system_type,energy_system_description,energy_density_class,power_class,tech_maturity_class,energy_system_extra_failure_risk,battery_mass_kg,battery_spec_energy_Wh_per_kg,battery_energy_Wh,battery_nominal_voltage_V,battery_max_power_W,supercap_mass_kg,supercap_energy_Wh,supercap_max_power_W,motor_type,motor_efficiency,esc_efficiency,esc_current_rating_A,structural_material,structural_material_class,structural_extra_failure_risk,rotor_blade_material,landing_gear_material,frame_stiffness_longitudinal,tendon_cable_fraction,gust_rejection_gain,landing_gear_mass_kg,max_touchdown_velocity_mps,cruise_speed_mps,climb_rate_mps,mode_count,mtow_kg,payload_to_aircraft_ratio,rule_empty_mass_ok,rule_payload_ok,design_qualifying,design_qualifying_score,design_summary,propulsion_architecture,primary_propulsor_type,secondary_propulsor_type,secondary_propulsor_fraction,propulsion_hover_power_factor,propulsion_cruise_power_factor,propulsion_arch_extra_failure_risk,wing_foldable,wing_deploy_time_s,wing_deploy_failure_risk,image_prompt,design_success_rate,design_qualifying_rate,design_rule_penalty_rate,design_rank_score,design_stars
+DLIFT_186142ea7d,harpy_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,21.26938124699791,57.34675561410429,6,2.1310596998296174,2.3533989748458226,18.16705265098237,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.797296377167434,182.38377755504564,1239.716590429023,39.74193418585944,9357.625783792062,0.07960790905159087,3.184316362063635,127.3726544825454,electric_brushless_outunner,0.8101439266950624,0.9743572358052935,50.17234716474934,carbon_composite,light_stiff,0.01,glass_composite,steel,0.49973927897133646,0.0,1.383898525813863,2.9997059385351537,0.512997519356122,21.11638503665616,4.792557579952907,4,78.6161368611022,2.6962117490934796,True,True,True,2.6962117490934796,"Bio-inspired by harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 21.3 kg, and carries a payload of 57.3 kg (2.70:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.8 kg battery (~1240 Wh usable) at about 40 V. Estimated battery peak power is ~9.4 kW. It also includes ~0.1 kg of supercapacitors (~3 Wh) that can provide high peak power (up to ~0.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~50 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 21.1 m/s and climbs at about 4.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.70. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, with 6 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_a2afffcfd2,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,18.72043005127034,65.17654082146296,6,2.4065631291911926,2.761728347372879,17.947594122237227,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.419721491215087,246.69959637118455,1090.343507955812,74.65487460629072,9273.480451249286,2.961699190894513,118.46796763578052,4738.718705431221,electric_brushless_outunner,0.8194458780041052,0.9494783344663124,43.97422856303852,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.5859998955209822,0.0,1.495083072449116,4.543506016493836,0.7685822287867354,7.308573408382044,2.4281439108376706,6,83.8969708727333,3.4815728400983064,True,True,True,3.4815728400983064,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 18.7 kg, and carries a payload of 65.2 kg (3.48:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.4 kg battery (~1090 Wh usable) at about 75 V. Estimated battery peak power is ~9.3 kW. It also includes ~3.0 kg of supercapacitors (~118 Wh) that can provide high peak power (up to ~4.7 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~44 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 7.3 m/s and climbs at about 2.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.48. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 6 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_1db7e6427c,"bat,bee,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,7,17.683741562706025,60.12501644221612,20,1.4895592618943285,2.9024082397211233,10.166602054898558,0.2087277287280303,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.741218349745656,184.16684865946044,1794.0094855763673,92.53821785149832,9002.338686328441,0.20585511135830825,8.23420445433233,329.3681781732932,electric_brushless_outunner,0.8158741175187062,0.9566002828445324,7.883475808776741,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.4967532282436646,0.0,1.7588432694268972,3.477077237467018,0.9770898837778117,14.471221218922562,2.4575577844372263,3,77.80875800492214,3.4000166892857253,True,True,True,3.4000166892857253,"Bio-inspired by bat, bee, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 17.7 kg, and carries a payload of 60.1 kg (3.40:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.7 kg battery (~1794 Wh usable) at about 93 V. Estimated battery peak power is ~9.0 kW. It also includes ~0.2 kg of supercapacitors (~8 Wh) that can provide high peak power (up to ~0.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~8 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~7.8 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 14.5 m/s and climbs at about 2.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.40. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,7.782408464607252,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, bee, golden_eagle, with 20 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_11dd30de89,"tiger,osprey,cheetah","LIFT_BURST_POWER,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,8,17.476451188404727,70.94750087366516,5,1.1404172194183286,2.260044554008121,16.588333465666,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,5.796751245540015,302.0511696699091,1750.915494000864,53.37532948487298,7034.906621906158,2.5242170448511065,100.96868179404426,4038.74727176177,electric_multirotor_plus_pusher,0.9090615409904187,0.9628708401216802,46.34843678492456,carbon_composite,light_stiff,0.01,aluminum,steel,0.44855776580981266,0.652857141953873,1.2,3.206455961119727,1.996471028806059,14.649991539157126,3.888879127613631,5,88.42395206206989,4.059605700769353,True,True,True,4.059605700769353,"Bio-inspired by tiger, osprey, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 17.5 kg, and carries a payload of 70.9 kg (4.06:1 payload-to-aircraft mass ratio). The energy system is li-s with a 5.8 kg battery (~1751 Wh usable) at about 53 V. Estimated battery peak power is ~7.0 kW. It also includes ~2.5 kg of supercapacitors (~101 Wh) that can provide high peak power (up to ~4.0 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~46 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; a compliant spine-like frame that absorbs dynamic loads; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 14.6 m/s and climbs at about 3.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.06. ",rotor_plus_pusher,multirotor,pusher_propeller,0.35343440529885994,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, cheetah, with 5 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_79104556e5,"albatross,osprey,bat","LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",3,8,19.05722469884954,52.05830458473068,12,1.390020318485322,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.827258840925902,233.14238213728922,2524.2929181904897,34.623900955783945,28031.71579727542,0.0,0.0,0.0,electric_multirotor_plus_pusher,0.8171514511654963,0.945704134467075,77.78233560277471,carbon_composite,light_stiff,0.01,aluminum,titanium,0.4300939412114464,0.0,1.2,0.9996659308393895,1.8221152851946336,5.515602995723967,2.0594413089228354,3,71.11552928358022,2.731683411796754,True,True,True,2.731683411796754,"Bio-inspired by albatross, osprey, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 19.1 kg, and carries a payload of 52.1 kg (2.73:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.8 kg battery (~2524 Wh usable) at about 35 V. Estimated battery peak power is ~28.0 kW. The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~78 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.7 s with a synthetic deployment failure risk of ~9.3%. In the synthetic mission model, it cruises at about 5.5 m/s and climbs at about 2.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.73. ",rotor_plus_pusher,multirotor,pusher_propeller,0.20631243340446412,1.05,0.9,0.01,True,2.68189584071928,0.09278882320895054,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, osprey, bat, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,0.9,0.019999999999999997,3
+DLIFT_ae222fd3a2,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,13.383179037696928,71.7073044688947,20,1.5164945575170312,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.236530173175778,226.27576535729497,1637.4514034665074,32.59416168221386,12317.335064326397,0.0,0.0,0.0,electric_multirotor_plus_micro_turbojet,0.8708887490633388,0.9558796655985721,28.068754366815885,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.4195147197243459,0.0,1.2,2.905032116884856,0.5038602435080877,8.536891634453221,2.796294334174036,6,85.09048350659164,5.358017274289906,True,True,True,5.358017274289906,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 13.4 kg, and carries a payload of 71.7 kg (5.36:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.2 kg battery (~1637 Wh usable) at about 33 V. Estimated battery peak power is ~12.3 kW. The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~28 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 8.5 m/s and climbs at about 2.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.36. ",rotor_plus_small_jet,multirotor,small_jet,0.13307976530145282,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 20 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.4,0.6,3
+DLIFT_3d85481be6,"osprey,cheetah,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",3,9,19.128037457262288,72.19392072628818,10,2.0317271900241836,2.5993411226066057,11.643474681708465,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.414499280374203,246.28742843642104,1087.2356755977937,82.70956164030078,11066.706290882521,2.6089990382485766,104.35996152994306,4174.398461197723,electric_multirotor_plus_pusher,0.7925877171122497,0.9491677628937116,25.36702542995526,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.6108284054085863,0.2674684590948292,1.2,3.23114552708662,2.4552410423802398,10.445949410178986,4.451289094829386,4,91.32195818355046,3.77424609751998,True,True,True,3.77424609751998,"Bio-inspired by osprey, cheetah, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 19.1 kg, and carries a payload of 72.2 kg (3.77:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.4 kg battery (~1087 Wh usable) at about 83 V. Estimated battery peak power is ~11.1 kW. It also includes ~2.6 kg of supercapacitors (~104 Wh) that can provide high peak power (up to ~4.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~25 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic mission model, it cruises at about 10.4 m/s and climbs at about 4.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.77. ",rotor_plus_pusher,multirotor,pusher_propeller,0.20698534075329356,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, cheetah, harpy_eagle, with 10 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_8216f68b93,"albatross,osprey,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,10,15.910899305941191,66.42393968335877,8,1.115110089158623,2.213972451807986,9.763298891263954,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,10.321585570293031,391.1053593970647,4036.8274340170133,43.686875322112094,15600.82436000075,1.4999931782205898,59.999727128823594,2399.9890851529435,electric_brushless_outunner,0.8956045176466855,0.9703911726061754,88.36705055848,steel_truss,heavy_robust,0.01,glass_composite,steel,0.3301771644018054,0.34114915079174846,1.4998424340249419,3.809062852100728,1.9568542146650123,7.089559946100321,3.083684268347892,4,82.33483898929995,4.174744519849724,True,True,True,4.174744519849724,"Bio-inspired by albatross, osprey, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 15.9 kg, and carries a payload of 66.4 kg (4.17:1 payload-to-aircraft mass ratio). The energy system is li-s with a 10.3 kg battery (~4037 Wh usable) at about 44 V. Estimated battery peak power is ~15.6 kW. It also includes ~1.5 kg of supercapacitors (~60 Wh) that can provide high peak power (up to ~2.4 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~88 A. The main frame uses steel truss (heavy_robust), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; multiple flight modes to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic mission model, it cruises at about 7.1 m/s and climbs at about 3.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.17. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, osprey, cheetah, with 8 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.1,0.1,0.9,0.1,3
+DLIFT_88212b4dde,"albatross,dragonfly,bat","LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",3,7,20.157045569162197,66.76734183211451,15,2.2810669291659202,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.355559282857166,244.29029040914637,1552.601422921723,95.1971835361851,9081.732915430897,0.0,0.0,0.0,electric_multirotor_plus_pusher,0.9003445977759189,0.9572228886366955,8.46103655578082,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.8742508561954588,0.0,1.2,3.242018326780159,0.9710539702317507,20.662003740529023,2.7004834720051805,2,86.9243874012767,3.312357537865586,True,True,True,3.312357537865586,"Bio-inspired by albatross, dragonfly, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 20.2 kg, and carries a payload of 66.8 kg (3.31:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.4 kg battery (~1553 Wh usable) at about 95 V. Estimated battery peak power is ~9.1 kW. The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~8 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency; long, high-aspect-ratio lifting surfaces for efficient cruise. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.9 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 20.7 m/s and climbs at about 2.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.31. ",rotor_plus_pusher,multirotor,pusher_propeller,0.22369911445687723,1.05,0.9,0.01,True,2.9279488564381584,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, dragonfly, bat, with 15 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.5,0.5,0.5,0.5,3
+DLIFT_057a49a2d7,"bee,dragonfly","LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",2,3,14.275730283320435,56.88266357992639,23,1.927836730905342,1.0,0.0,0.09958999458608006,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.796867543966723,237.9667543189523,2807.2622805683513,56.93455475063206,23855.104229438195,0.0,0.0,0.0,electric_multirotor_plus_pusher,0.8067754612404923,0.9797286089853857,14.197217373503412,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.3460683865418145,0.0,1.2,0.5965981359837482,1.135375140731193,14.31458401905105,4.854411738713141,3,71.15839386324683,3.9845711883746713,True,True,True,3.9845711883746713,"Bio-inspired by bee, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 14.3 kg, and carries a payload of 56.9 kg (3.98:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.8 kg battery (~2807 Wh usable) at about 57 V. Estimated battery peak power is ~23.9 kW. The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~14 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include unsteady aerodynamics for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 14.3 m/s and climbs at about 4.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.98. ",rotor_plus_pusher,multirotor,pusher_propeller,0.3685419621733098,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, dragonfly, with 23 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.0,0.8400000000000001,5
+DLIFT_89b5f0b8fd,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,14.307635123948849,65.28117873011281,11,2.0666476925171366,1.5307205082286268,3.093597499791908,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.098648236006788,220.36470675600566,2445.7503639156953,33.184237203946424,9199.101240133648,0.1756745260500162,7.026981042000648,281.0792416800259,electric_brushless_outunner,0.7927478034438985,0.9705882522928344,44.58204558232767,steel_truss,heavy_robust,0.01,carbon_composite,composite,0.39914345520443933,0.3698356378836447,1.6736044361563045,2.6743125922426825,0.9369584736014052,12.230880992211645,5.091994946237292,5,79.58881385406167,4.562681265252694,True,True,True,4.562681265252694,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 14.3 kg, and carries a payload of 65.3 kg (4.56:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.1 kg battery (~2446 Wh usable) at about 33 V. Estimated battery peak power is ~9.2 kW. It also includes ~0.2 kg of supercapacitors (~7 Wh) that can provide high peak power (up to ~0.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~45 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 12.2 m/s and climbs at about 5.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.56. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 11 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.3,0.62,4
+DLIFT_4c746a3773,"osprey,cheetah,bat,tiger,bee","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,12,19.668985545680354,64.21527034762549,9,1.4663585548424254,2.9801176971368872,6.611546358290086,0.12536246077049995,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.742372186323412,252.88429865209685,1199.2714642856072,83.55751218287992,14010.139778873445,0.5105744196438294,20.42297678575318,816.9190714301271,electric_brushless_outunner,0.8049454246480958,0.9798134332199608,24.46481478497737,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.5209571853870477,0.2071824043582631,1.2,2.8800754740957726,2.1918968677866966,23.544221761981138,2.446615110974248,6,83.88425589330585,3.2647982885791618,True,True,True,3.2647982885791618,"Bio-inspired by osprey, cheetah, bat, tiger, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 19.7 kg, and carries a payload of 64.2 kg (3.26:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.7 kg battery (~1199 Wh usable) at about 84 V. Estimated battery peak power is ~14.0 kW. It also includes ~0.5 kg of supercapacitors (~20 Wh) that can provide high peak power (up to ~0.8 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~24 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; multiple flight modes to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; a compliant spine-like frame that absorbs dynamic loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~7.0 s with a synthetic deployment failure risk of ~11.2%. In the synthetic mission model, it cruises at about 23.5 m/s and climbs at about 2.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.26. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,6.958097165468221,0.11221063973326463,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, cheetah, bat, tiger, bee, with 9 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_b1ace449e9,bee,"LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST",1,2,20.166255092990546,66.30958546888877,8,2.2676520310764494,1.0,0.0,0.10323908768740103,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.001229949136345,253.2883178237435,2533.1947099851886,51.62954961962532,13511.292522330752,0.0,0.0,0.0,electric_ducted_fan,0.8118649806481142,0.9623590451367736,55.95361587442322,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.6172663006222474,0.0,1.8047908608178405,1.4262462868818,1.6344979683049392,15.225991961899073,5.298734750390599,5,86.47584056187932,3.28814572478243,True,True,True,3.28814572478243,"Bio-inspired by bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 20.2 kg, and carries a payload of 66.3 kg (3.29:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.0 kg battery (~2533 Wh usable) at about 52 V. Estimated battery peak power is ~13.5 kW. The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~56 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include unsteady aerodynamics for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy. In the synthetic mission model, it cruises at about 15.2 m/s and climbs at about 5.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.29. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, with 8 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.2,0.64,4
+DLIFT_38efeba5d9,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,17.648951020552623,66.5931629528602,15,2.4915977361147545,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.905006265652736,247.40124573225373,1955.7083976437577,50.61252568733518,12612.696711928897,0.0,0.0,0.0,electric_brushless_outunner,0.8902978201021287,0.9671452674348426,22.85537666644568,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.9913630023771032,0.0,1.2,3.412294077566113,1.5103328410093135,7.1769375754333,3.4417499211869655,5,84.24211397341281,3.773207986996557,True,True,True,3.773207986996557,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 17.6 kg, and carries a payload of 66.6 kg (3.77:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.9 kg battery (~1956 Wh usable) at about 51 V. Estimated battery peak power is ~12.6 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~23 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 7.2 m/s and climbs at about 3.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.77. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 15 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.4,0.4,0.6,0.4,3
+DLIFT_486bdfbbb3,"harpy_eagle,cheetah,dragonfly,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,10,18.02881361842205,58.602044692932196,11,1.8036861707592111,2.6013877687316,14.579433327345903,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.151912359433921,192.12359261935,605.556726115777,73.38483960604603,4697.288074140528,1.0269874688665805,41.07949875466322,1643.179950186529,electric_multirotor_plus_micro_turbojet,0.8204924828379997,0.9755121477318068,7.112155503034391,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.5236885471678664,0.15146041152910883,1.6399417633833202,0.5794789064162083,0.7246450159255677,23.724713545384365,2.1015663112006964,4,76.63085831135425,3.250465944861283,True,True,True,3.250465944861283,"Bio-inspired by harpy_eagle, cheetah, dragonfly, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 18.0 kg, and carries a payload of 58.6 kg (3.25:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.2 kg battery (~606 Wh usable) at about 73 V. Estimated battery peak power is ~4.7 kW. It also includes ~1.0 kg of supercapacitors (~41 Wh) that can provide high peak power (up to ~1.6 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~7 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy. It uses foldable wings that deploy after takeoff. The wing deployment time is ~8.0 s with a synthetic deployment failure risk of ~10.2%. In the synthetic mission model, it cruises at about 23.7 m/s and climbs at about 2.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.25. ",rotor_plus_small_jet,multirotor,small_jet,0.25001237281728605,1.15,0.85,0.03,True,7.988080380013134,0.10241047911171895,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, cheetah, dragonfly, bat, with 11 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_db3d1b584a,tiger,"LIFT_BURST_POWER,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",1,3,15.120900424703368,76.6760046125009,9,2.324839958041488,2.8656343310160817,12.363818738622856,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.823369443436642,206.4002650454944,1614.7455266741447,54.18302489889506,9037.259898027414,0.7888281503175874,31.553126012703494,1262.1250405081398,electric_multirotor_plus_pusher,0.8444388659876513,0.98450958702927,19.6932169603362,carbon_composite,light_stiff,0.01,aluminum,titanium,0.5158153187788781,0.5684312803042366,1.8396249706009744,2.5521672039122767,2.706218246648995,11.468812809640841,3.0743412431571455,5,91.79690503720427,5.070862346744478,True,True,True,5.070862346744478,"Bio-inspired by tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 15.1 kg, and carries a payload of 76.7 kg (5.07:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.8 kg battery (~1615 Wh usable) at about 54 V. Estimated battery peak power is ~9.0 kW. It also includes ~0.8 kg of supercapacitors (~32 Wh) that can provide high peak power (up to ~1.3 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~20 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 11.5 m/s and climbs at about 3.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.07. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4645420400546136,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_b0ca104c3d,"bee,harpy_eagle,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,6,21.39828666409742,68.67714195888759,8,1.1000872256738221,2.8761431819149523,12.434810912609613,0.18536019793394523,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.112356858482098,186.36421705421273,1139.1246002869636,88.93004219881581,8785.84718832309,0.19173164880172455,7.669265952068982,306.77063808275926,electric_brushless_outunner,0.9161082073579703,0.9470873749979513,16.284641294858623,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.6625955440308804,0.0,1.2,3.000813492682828,0.5178227595013085,18.08674089331795,3.992863666143449,5,90.07542862298502,3.209469198957682,True,True,True,3.209469198957682,"Bio-inspired by bee, harpy_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 21.4 kg, and carries a payload of 68.7 kg (3.21:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.1 kg battery (~1139 Wh usable) at about 89 V. Estimated battery peak power is ~8.8 kW. It also includes ~0.2 kg of supercapacitors (~8 Wh) that can provide high peak power (up to ~0.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~16 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 18.1 m/s and climbs at about 4.0 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.21. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, harpy_eagle, dragonfly, with 8 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_f6f79ee1e4,"bat,dragonfly,bee,tiger,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,10,19.579235523687935,70.44779070819837,9,1.6672174856259838,1.446503075388187,10.227113285050716,0.05577980210822733,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.6739118822437,250.5834197955689,2173.5385024580464,77.21169501669294,11701.888359138391,1.3686694952950538,54.74677981180215,2189.871192472086,electric_brushless_outunner,0.7910275855543923,0.9817414940485732,33.20449034494149,steel_truss,heavy_robust,0.01,glass_composite,titanium,0.4446703106884283,0.5990576051934245,1.2,2.79539422101758,1.8719149724336428,8.449114686320963,2.342772567522218,3,90.02702623188631,3.5980868927679595,True,True,True,3.5980868927679595,"Bio-inspired by bat, dragonfly, bee, tiger, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 19.6 kg, and carries a payload of 70.4 kg (3.60:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.7 kg battery (~2174 Wh usable) at about 77 V. Estimated battery peak power is ~11.7 kW. It also includes ~1.4 kg of supercapacitors (~55 Wh) that can provide high peak power (up to ~2.2 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~33 A. The main frame uses steel truss (heavy_robust), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. It uses foldable wings that deploy after takeoff. The wing deployment time is ~5.1 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 8.4 m/s and climbs at about 2.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.60. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,5.072042273200874,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, dragonfly, bee, tiger, harpy_eagle, with 9 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.4,0.4,0.5,0.42000000000000004,3
+DLIFT_27f2558c87,"cheetah,bat,bee,harpy_eagle,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,13,22.271565476725804,77.09729392764254,12,1.1122106537652272,1.1004439597634048,12.671633058357482,0.12584693475312117,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.931274715818876,240.3867226177506,2868.1200255877334,75.43092375153742,34319.47358321937,0.001856577766594203,0.07426311066376812,2.9705244265507247,electric_ducted_fan,0.8497766819362277,0.959857563798165,55.6204059333152,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.7,0.13781026504828414,0.5155489701625924,1.2351740004822602,0.750532324061137,6.184254463367413,3.8305472608484994,4,99.36885940436835,3.461691725631529,True,True,True,3.461691725631529,"Bio-inspired by cheetah, bat, bee, harpy_eagle, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 22.3 kg, and carries a payload of 77.1 kg (3.46:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.9 kg battery (~2868 Wh usable) at about 75 V. Estimated battery peak power is ~34.3 kW. It also includes ~0.0 kg of supercapacitors (~0 Wh) that can provide high peak power (up to ~0.0 kW). The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~56 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; multiple flight modes to optimize heavy-load and unloaded segments. It uses foldable wings that deploy after takeoff. The wing deployment time is ~3.6 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 6.2 m/s and climbs at about 3.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.46. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,True,3.5517221264504197,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, bat, bee, harpy_eagle, albatross, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.3,0.3,0.7,0.30000000000000004,3
+DLIFT_b41fd13bc7,"golden_eagle,bat,dragonfly,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,7,15.969598319937454,68.18608015428786,18,2.046573749328595,1.3780598286407957,17.194407466579054,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.0845169654016535,245.12517465012786,1246.3431091556185,66.32163491938405,3832.0233883184396,2.4901022798155608,99.60409119262243,3984.1636477048974,electric_brushless_outunner,0.8753913611838491,0.9461415501377957,9.978917029349153,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.5816696619822739,0.0,1.2,3.703687367098205,2.434197944042618,24.424846787392287,2.5956584046668887,4,84.15567847422531,4.269742969624982,True,True,True,4.269742969624982,"Bio-inspired by golden_eagle, bat, dragonfly, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 16.0 kg, and carries a payload of 68.2 kg (4.27:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.1 kg battery (~1246 Wh usable) at about 66 V. Estimated battery peak power is ~3.8 kW. It also includes ~2.5 kg of supercapacitors (~100 Wh) that can provide high peak power (up to ~4.0 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~10 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~5.5 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 24.4 m/s and climbs at about 2.6 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.27. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,5.462376566820006,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, bat, dragonfly, harpy_eagle, with 18 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_3cce5ab9fe,bat,"WING_FOLDABLE,WING_MORPHING_MEMBRANE",1,2,12.127698985639972,79.42424194516539,12,1.536119521337032,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.055398956812782,185.79996202458943,939.292934194964,39.8617087518247,8577.873446274974,0.0,0.0,0.0,electric_brushless_outunner,0.8551894491426064,0.9671419394149637,25.170721377528114,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.6043404172533214,0.0,1.8222713717372006,2.062529599948411,1.4137828544181552,7.492513258112011,5.214710584698231,5,91.55194093080536,6.548995158868071,True,True,True,6.548995158868071,"Bio-inspired by bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 12.1 kg, and carries a payload of 79.4 kg (6.55:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.1 kg battery (~939 Wh usable) at about 40 V. Estimated battery peak power is ~8.6 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~25 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include foldable wings that deploy after vertical takeoff for cruise efficiency; morphing lifting surface that can change camber and area for control and efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~7.0 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 7.5 m/s and climbs at about 5.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 6.55. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,7.036774697707835,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.1,0.1,0.9,0.1,3
+DLIFT_814701bf4d,"albatross,bat,osprey,harpy_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",4,11,23.006515187242623,69.85951747118625,4,1.9663163328352748,1.2881881973630325,6.954759412341261,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,6.820335900063088,319.2573253474882,2177.4421974255947,82.53754887512596,10174.633595677566,2.28131696574739,91.2526786298956,3650.107145195824,electric_brushless_outunner,0.7909677023982638,0.9482831711740564,50.4656693760949,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.9485668798799226,0.0,1.55059294018935,3.2695702022857303,1.2880392461176247,17.319907662645324,2.4690526973086584,5,92.86603265842888,3.036510175601221,True,True,True,3.036510175601221,"Bio-inspired by albatross, bat, osprey, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 23.0 kg, and carries a payload of 69.9 kg (3.04:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 6.8 kg battery (~2177 Wh usable) at about 83 V. Estimated battery peak power is ~10.2 kW. It also includes ~2.3 kg of supercapacitors (~91 Wh) that can provide high peak power (up to ~3.7 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~50 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight. It uses foldable wings that deploy after takeoff. The wing deployment time is ~8.0 s with a synthetic deployment failure risk of ~11.4%. In the synthetic mission model, it cruises at about 17.3 m/s and climbs at about 2.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.04. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,7.977568387805238,0.11383174831273886,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, bat, osprey, harpy_eagle, with 4 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.3,0.62,4
+DLIFT_34bc718f10,albatross,"LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_HIGH_ASPECT",1,3,22.919185093537088,70.78698032469944,7,2.2675926236222805,1.0,0.0,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,4.159404345779832,340.1276031674729,1414.728230734465,34.88961547554334,4364.897045286525,0.0,0.0,0.0,electric_brushless_outunner,0.9171720239633913,0.982104694864923,24.78087423057955,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.801242318063119,0.0,0.9757363584059431,3.4182357617987513,0.8220787512537744,5.4469180638223875,5.69618782029343,6,93.70616541823654,3.088546998325017,True,True,True,3.088546998325017,"Bio-inspired by albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 22.9 kg, and carries a payload of 70.8 kg (3.09:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 4.2 kg battery (~1415 Wh usable) at about 35 V. Estimated battery peak power is ~4.4 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~25 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic mission model, it cruises at about 5.4 m/s and climbs at about 5.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.09. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, with 7 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_12e138b90e,"harpy_eagle,golden_eagle,tiger,albatross,bee","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,10,22.406737838864373,56.8891645821312,8,2.026293616155917,1.34100084504493,12.665735917512212,0.14302681779537907,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.050231178522228,224.91918109567848,1135.8938610170828,47.47447518132729,13329.833893962226,2.545606411296364,101.82425645185455,4072.9702580741823,electric_multirotor_plus_micro_turbojet,0.8395160876777746,0.9730841412358169,60.0483140432888,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.3917760752457585,0.4624104180742219,0.9722286675357257,4.02332905386507,1.8453072956360272,16.44972283661818,2.7735013169520504,6,79.29590242099557,2.5389311461241464,True,True,True,2.5389311461241464,"Bio-inspired by harpy_eagle, golden_eagle, tiger, albatross, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 22.4 kg, and carries a payload of 56.9 kg (2.54:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.1 kg battery (~1136 Wh usable) at about 47 V. Estimated battery peak power is ~13.3 kW. It also includes ~2.5 kg of supercapacitors (~102 Wh) that can provide high peak power (up to ~4.1 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~60 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 16.4 m/s and climbs at about 2.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.54. ",rotor_plus_small_jet,multirotor,small_jet,0.20550246772593425,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, golden_eagle, tiger, albatross, bee, with 8 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.2,0.8,5
+DLIFT_4ef9cdc7af,"tiger,osprey,bee","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,8,16.323724776837494,67.02698196612721,21,1.7907350434176956,2.654366876292502,12.50924175948381,0.22496194015380605,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,8.373312267069295,331.75847848712857,2777.9173376205185,52.17887155026996,13362.766554590824,0.14482004271566185,5.792801708626474,231.71206834505895,electric_multirotor_plus_pusher,0.8032697249737734,0.976847529799143,10.025616338708174,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.8862533245562922,0.6917957802705726,1.2,4.4189131281035205,2.6257421164089765,15.962657781497976,4.1231784444016935,6,83.3507067429647,4.106108310600468,True,True,True,4.106108310600468,"Bio-inspired by tiger, osprey, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 21 rotors, has an empty mass of 16.3 kg, and carries a payload of 67.0 kg (4.11:1 payload-to-aircraft mass ratio). The energy system is li-s with a 8.4 kg battery (~2778 Wh usable) at about 52 V. Estimated battery peak power is ~13.4 kW. It also includes ~0.1 kg of supercapacitors (~6 Wh) that can provide high peak power (up to ~0.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~10 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 16.0 m/s and climbs at about 4.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.11. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4015410411275828,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, bee, with 21 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_829bd436cb,"bee,bat,tiger,albatross,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,12,15.434551146497753,64.34521508932265,13,2.1669512313418418,2.815614067360076,11.100230469237538,0.10729711330576253,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.43141496016827,228.86311024728485,1014.1874105804583,74.10864166337348,4117.580862382357,0.42808481269248555,17.12339250769942,684.9357003079768,electric_brushless_outunner,0.8680420839366908,0.9761457065828827,7.379839969735522,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.670622695500784,0.13387099246198925,0.5297311009822636,2.806983213484509,2.4500516620794555,13.76527618821251,3.8487493238512553,6,79.7797662358204,4.16890743880966,True,True,True,4.16890743880966,"Bio-inspired by bee, bat, tiger, albatross, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 15.4 kg, and carries a payload of 64.3 kg (4.17:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.4 kg battery (~1014 Wh usable) at about 74 V. Estimated battery peak power is ~4.1 kW. It also includes ~0.4 kg of supercapacitors (~17 Wh) that can provide high peak power (up to ~0.7 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~7 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.7 s with a synthetic deployment failure risk of ~11.9%. In the synthetic mission model, it cruises at about 13.8 m/s and climbs at about 3.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.17. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,2.699526242122687,0.11861608225621768,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, bat, tiger, albatross, cheetah, with 13 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_9b778c93da,"harpy_eagle,golden_eagle,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,5,14.480848878314234,75.78327513319701,9,1.3949333702463107,1.4763986800541355,18.81449849683375,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.52258313105362,181.42815902341218,2090.5210446612828,49.29671239283205,19334.69185090772,2.8930628794508455,115.72251517803382,4628.900607121353,electric_multirotor_plus_micro_turbojet,0.863020655654842,0.9630552041667737,54.68791126539679,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.8080785899064118,0.0,1.7507262318264105,1.5773619690861482,1.0352575365989751,22.67317243485641,3.745758853258297,2,90.26412401151124,5.2333447969812115,True,True,True,5.2333447969812115,"Bio-inspired by harpy_eagle, golden_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 14.5 kg, and carries a payload of 75.8 kg (5.23:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.5 kg battery (~2091 Wh usable) at about 49 V. Estimated battery peak power is ~19.3 kW. It also includes ~2.9 kg of supercapacitors (~116 Wh) that can provide high peak power (up to ~4.6 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~55 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 22.7 m/s and climbs at about 3.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.23. ",rotor_plus_small_jet,multirotor,small_jet,0.3064317558128567,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, golden_eagle, dragonfly, with 9 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.0,0.76,4
+DLIFT_4a0441255d,"bat,tiger,cheetah,osprey","LIFT_BURST_POWER,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,10,17.564725969276495,57.39922297989158,7,2.0161785443354496,1.96349917750908,6.256020945010497,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.709094929433679,232.3508859951873,2255.9168090652956,40.28568702160351,6808.791039258336,2.4068407980709634,96.27363192283853,3850.9452769135414,electric_multirotor_plus_micro_turbojet,0.7908344878130301,0.9809202693914906,36.56752990169221,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.48839096030218204,0.6656374734548174,1.2,3.5484310940395454,3.027221396205491,9.306042387905238,3.4602824011127935,5,74.96394894916807,3.267868971044124,True,True,True,3.267868971044124,"Bio-inspired by bat, tiger, cheetah, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 17.6 kg, and carries a payload of 57.4 kg (3.27:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.7 kg battery (~2256 Wh usable) at about 40 V. Estimated battery peak power is ~6.8 kW. It also includes ~2.4 kg of supercapacitors (~96 Wh) that can provide high peak power (up to ~3.9 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~37 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; a compliant spine-like frame that absorbs dynamic loads; enhanced gust rejection and stability control for windy conditions. It uses foldable wings that deploy after takeoff. The wing deployment time is ~3.5 s with a synthetic deployment failure risk of ~8.2%. In the synthetic mission model, it cruises at about 9.3 m/s and climbs at about 3.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.27. ",rotor_plus_small_jet,multirotor,small_jet,0.2288257471911092,1.15,0.85,0.03,True,3.51783393849316,0.08157653903958685,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, tiger, cheetah, osprey, with 7 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_4978502884,"bee,dragonfly,golden_eagle,harpy_eagle,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,8,14.453676435596694,66.3892408982291,22,1.2283925731634804,2.1786985126880323,6.866239754659469,0.1960447617027045,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.3401325911889845,244.39807088278596,1060.720032662095,44.13727496126515,12247.124331883235,0.1458025307541322,5.8321012301652875,233.28404920661148,electric_brushless_outunner,0.8441658472266843,0.9548217153233688,22.10308413307849,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.4847264079661402,0.0,1.2,1.8754514314092452,2.2481152570392853,15.127451244009578,5.3066789122856495,6,80.8429173338258,4.593242500899277,True,True,True,4.593242500899277,"Bio-inspired by bee, dragonfly, golden_eagle, harpy_eagle, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 14.5 kg, and carries a payload of 66.4 kg (4.59:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.3 kg battery (~1061 Wh usable) at about 44 V. Estimated battery peak power is ~12.2 kW. It also includes ~0.1 kg of supercapacitors (~6 Wh) that can provide high peak power (up to ~0.2 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~22 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.2 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 15.1 m/s and climbs at about 5.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.59. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,6.153558396544535,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, dragonfly, golden_eagle, harpy_eagle, bat, with 22 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.1,0.1,0.9,0.1,3
+DLIFT_f8b670a07c,harpy_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,16.44685661832859,70.59062180503032,7,1.3301502666882274,2.535572496774625,14.478243637905525,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.739139718415245,206.8649569426758,2221.551675451349,82.25310517845716,10622.44272088218,1.4480331088392346,57.92132435356939,2316.8529741427756,electric_brushless_outunner,0.7863532847692426,0.9578381459149035,37.4163793117556,titanium_alloy,heavy_robust,0.005,carbon_composite,steel,0.34885813665700444,0.0,0.5532245631224951,4.738767524802025,1.5507313097450037,13.218418747955948,2.730568163310761,6,87.03747842335892,4.292043363858552,True,True,True,4.292043363858552,"Bio-inspired by harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 16.4 kg, and carries a payload of 70.6 kg (4.29:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.7 kg battery (~2222 Wh usable) at about 82 V. Estimated battery peak power is ~10.6 kW. It also includes ~1.4 kg of supercapacitors (~58 Wh) that can provide high peak power (up to ~2.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~37 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 13.2 m/s and climbs at about 2.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.29. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, with 7 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_25c26fb42c,"dragonfly,albatross,tiger","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,8,15.995681115826853,75.97503879428092,19,2.4705186868245885,1.8376181958215048,11.224199235915043,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.256297669729904,222.19073985530014,2278.854367413478,52.89758331332297,9888.495520578577,1.9876458093348761,79.50583237339504,3180.2332949358015,electric_multirotor_plus_pusher,0.8987148922077668,0.9790898101198189,8.6481937119795,steel_truss,heavy_robust,0.01,glass_composite,composite,0.8294200095308542,0.597706804688054,1.893122264083288,6.045638834281318,1.6490081158776544,13.829272989488006,2.9168548681846387,2,91.97071991010777,4.7497220183458,True,True,True,4.7497220183458,"Bio-inspired by dragonfly, albatross, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 16.0 kg, and carries a payload of 76.0 kg (4.75:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.3 kg battery (~2279 Wh usable) at about 53 V. Estimated battery peak power is ~9.9 kW. It also includes ~2.0 kg of supercapacitors (~80 Wh) that can provide high peak power (up to ~3.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~9 A. The main frame uses steel truss (heavy_robust), with glass composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads. In the synthetic mission model, it cruises at about 13.8 m/s and climbs at about 2.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.75. ",rotor_plus_pusher,multirotor,pusher_propeller,0.504371484864935,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, albatross, tiger, with 19 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_e9ad73c0f6,"dragonfly,bat,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,7,18.653225939403292,56.9659552678647,12,2.2921633647006403,1.0054048909016895,13.268476207418754,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.056508693247424,219.36542503372658,1547.9540287484076,90.51561182449467,17012.002618540282,0.0139580252904693,0.558321011618772,22.33284046475088,electric_brushless_outunner,0.8697800859369388,0.9420853962679628,20.97406112317167,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.7034690437261657,0.0,1.8916731370194708,1.5629246138011592,0.5521248751234078,15.888105388621817,4.806687589516683,5,75.61918120726799,3.0539465641451944,True,True,True,3.0539465641451944,"Bio-inspired by dragonfly, bat, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 18.7 kg, and carries a payload of 57.0 kg (3.05:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.1 kg battery (~1548 Wh usable) at about 91 V. Estimated battery peak power is ~17.0 kW. It also includes ~0.0 kg of supercapacitors (~1 Wh) that can provide high peak power (up to ~0.0 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~21 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.0 s with a synthetic deployment failure risk of ~10.4%. In the synthetic mission model, it cruises at about 15.9 m/s and climbs at about 4.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.05. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,5.974517073001941,0.10404795301816996,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, bat, golden_eagle, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.3,0.62,4
+DLIFT_dbbb544516,"cheetah,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",2,6,16.78365499961696,56.989722315066906,8,2.327031790293233,2.4955571230503297,17.349052043142205,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus lithium-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,3.995785724701763,668.0975800236549,2669.5747729663144,53.76518531974992,10791.785149885609,2.1476463713302176,85.90585485320871,3436.2341941283485,electric_multirotor_plus_pusher,0.7960321476702706,0.9708140654354517,21.496996948214644,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.7,0.17321755683596796,1.5186096587538822,0.7729711264322219,2.3384584185276776,12.61247670914262,5.3684255310447675,5,73.77337731468387,3.3955489621520187,True,True,True,3.3955489621520187,"Bio-inspired by cheetah, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 16.8 kg, and carries a payload of 57.0 kg (3.40:1 payload-to-aircraft mass ratio). The energy system is fuel-cell-li-ion-hybrid with a 4.0 kg battery (~2670 Wh usable) at about 54 V. Estimated battery peak power is ~10.8 kW. It also includes ~2.1 kg of supercapacitors (~86 Wh) that can provide high peak power (up to ~3.4 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~21 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 12.6 m/s and climbs at about 5.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.40. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5903781211693315,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, harpy_eagle, with 8 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_d20dbfca98,"bee,harpy_eagle,bat,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,10,20.56672542637412,65.13079105651596,24,1.9096998506228808,2.2010905275210404,14.35605318693031,0.22034803832710978,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.549051854727386,247.12276597242158,1618.4198088370492,30.859821524009128,6025.245152368607,2.223523130350398,88.94092521401592,3557.637008560637,electric_brushless_outunner,0.8421423629428543,0.9695621259663975,17.00537315819906,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.7,0.5013032159155562,0.7283870832405595,0.6754736358766389,1.9025258946382921,23.052093176024265,3.1243102930908813,4,85.69751648289008,3.166804131735735,True,True,True,3.166804131735735,"Bio-inspired by bee, harpy_eagle, bat, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 24 rotors, has an empty mass of 20.6 kg, and carries a payload of 65.1 kg (3.17:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.5 kg battery (~1618 Wh usable) at about 31 V. Estimated battery peak power is ~6.0 kW. It also includes ~2.2 kg of supercapacitors (~89 Wh) that can provide high peak power (up to ~3.6 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~17 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.0 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 23.1 m/s and climbs at about 3.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.17. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,2.018715405029284,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, harpy_eagle, bat, cheetah, with 24 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_6c3d0f7b97,"bat,harpy_eagle,albatross,bee","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",4,10,21.12217046668799,78.50930720774214,15,1.16139321877069,2.622276952589737,19.237098771399147,0.2107120121228217,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,10.798352085433839,422.51306889356886,4562.444878609921,92.79370895738762,18524.601768194385,0.8154785889727143,32.619143558908576,1304.765742356343,electric_brushless_outunner,0.8226190869577114,0.9518136918157905,22.623088061164225,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.9603940277375822,0.0,0.7640496978590247,2.2741497900113044,1.6728282056367842,13.796548271521909,5.79536969022831,2,99.63147767443013,3.716914761745723,True,True,True,3.716914761745723,"Bio-inspired by bat, harpy_eagle, albatross, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 21.1 kg, and carries a payload of 78.5 kg (3.72:1 payload-to-aircraft mass ratio). The energy system is li-s with a 10.8 kg battery (~4562 Wh usable) at about 93 V. Estimated battery peak power is ~18.5 kW. It also includes ~0.8 kg of supercapacitors (~33 Wh) that can provide high peak power (up to ~1.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~23 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.1 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 13.8 m/s and climbs at about 5.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.72. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,2.1125135637857406,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, harpy_eagle, albatross, bee, with 15 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_c4b007f870,bat,"WING_FOLDABLE,WING_MORPHING_MEMBRANE",1,2,23.595577448362395,75.37553520027058,11,2.205716621920121,1.0,0.0,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,7.3945628461837485,288.4446663663039,2132.922213092138,64.31446614987402,8314.78309213308,0.0,0.0,0.0,electric_brushless_outunner,0.8484680174534317,0.9656654278530137,14.835095155127261,aluminum_lithium,medium_stiff,0.02,glass_composite,steel,0.9562112722140361,0.0,0.6381764269375927,2.544666311020279,0.6792552969043477,16.574483498860282,2.2241754091061474,4,98.97111264863297,3.194477243255679,True,True,True,3.194477243255679,"Bio-inspired by bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 23.6 kg, and carries a payload of 75.4 kg (3.19:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 7.4 kg battery (~2133 Wh usable) at about 64 V. Estimated battery peak power is ~8.3 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~15 A. The main frame uses aluminum lithium (medium_stiff), with glass composite rotor blades and steel landing gear. Key bio-inspired features include foldable wings that deploy after vertical takeoff for cruise efficiency; morphing lifting surface that can change camber and area for control and efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~3.8 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 16.6 m/s and climbs at about 2.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.19. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,3.8439103151307656,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, with 11 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_0fc40346e6,"cheetah,golden_eagle,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",3,6,15.335533640301284,72.41885618006305,4,1.1648535921606806,1.1281187047588652,3.970699555856296,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.496554294332867,199.8393650553636,2297.464110503994,26.686409605746675,7689.157814816272,2.8773560798220186,115.09424319288074,4603.769727715229,electric_multirotor_plus_pusher,0.8362995173114475,0.9608545327581896,149.9771131222425,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.3661498819927616,0.5123354358215375,0.5730280750153451,4.4387024531679184,0.8602434811333934,19.19972559864852,2.9372666228613737,4,87.75438982036432,4.722291240635321,True,True,True,4.722291240635321,"Bio-inspired by cheetah, golden_eagle, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 15.3 kg, and carries a payload of 72.4 kg (4.72:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.5 kg battery (~2297 Wh usable) at about 27 V. Estimated battery peak power is ~7.7 kW. It also includes ~2.9 kg of supercapacitors (~115 Wh) that can provide high peak power (up to ~4.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~150 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 19.2 m/s and climbs at about 2.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.72. ",rotor_plus_pusher,multirotor,pusher_propeller,0.23617050404778045,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, golden_eagle, harpy_eagle, with 4 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.1,0.8200000000000001,5
+DLIFT_0b4c9cc8d7,"tiger,dragonfly,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,7,16.494479680807295,56.01664106242188,8,2.243640443782935,2.0623459930808408,9.536677924874262,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,9.995778755110496,320.87348841695865,3207.380398596429,87.82629818124789,24394.8380294695,1.3844330997811254,55.377323991245014,2215.0929596498004,electric_multirotor_plus_pusher,0.8475655431969151,0.9738168528390261,30.027339602819467,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.5620929520778707,0.47308745915000866,1.2,2.7096622372119334,3.0597350842553697,20.68974232558601,3.3781578422733824,6,72.51112074322918,3.3960841533911448,True,True,True,3.3960841533911448,"Bio-inspired by tiger, dragonfly, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 16.5 kg, and carries a payload of 56.0 kg (3.40:1 payload-to-aircraft mass ratio). The energy system is li-s with a 10.0 kg battery (~3207 Wh usable) at about 88 V. Estimated battery peak power is ~24.4 kW. It also includes ~1.4 kg of supercapacitors (~55 Wh) that can provide high peak power (up to ~2.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~30 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads. In the synthetic mission model, it cruises at about 20.7 m/s and climbs at about 3.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.40. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5435239692046777,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, dragonfly, golden_eagle, with 8 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.9,0.9,0.1,0.9000000000000001,5
+DLIFT_1c14cd3673,"golden_eagle,dragonfly,osprey,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",4,10,18.104282902614994,58.88104828353365,17,1.810812962475532,1.2275052329540166,7.470853121738988,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus lithium-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,5.895799361635312,607.9936496904727,3584.6085717234123,74.75007011769912,13538.022146225738,1.5878026578771167,63.512106315084665,2540.4842526033867,electric_brushless_outunner,0.8376813771029142,0.9790564090590176,16.940677762312333,titanium_alloy,heavy_robust,0.005,glass_composite,steel,0.48688030026308776,0.42569996699954876,1.2376606470692497,3.2830417095781095,2.172387540864718,8.824848678165957,3.9731068266716503,4,76.98533118614864,3.2523270101479045,True,True,True,3.2523270101479045,"Bio-inspired by golden_eagle, dragonfly, osprey, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 17 rotors, has an empty mass of 18.1 kg, and carries a payload of 58.9 kg (3.25:1 payload-to-aircraft mass ratio). The energy system is fuel-cell-li-ion-hybrid with a 5.9 kg battery (~3585 Wh usable) at about 75 V. Estimated battery peak power is ~13.5 kW. It also includes ~1.6 kg of supercapacitors (~64 Wh) that can provide high peak power (up to ~2.5 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~17 A. The main frame uses titanium alloy (heavy_robust), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic mission model, it cruises at about 8.8 m/s and climbs at about 4.0 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.25. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, dragonfly, osprey, cheetah, with 17 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.4,0.4,0.4,0.44000000000000006,3
+DLIFT_e370562b10,"osprey,cheetah,harpy_eagle,tiger,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",5,10,15.50632912554579,50.26495863492862,8,1.7544470223439421,1.5443650070509725,7.650864790661273,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.64159291052648,215.19872686745816,1429.2623387172346,84.32941640374509,9772.700973328207,2.0513118751108763,82.05247500443505,3282.099000177402,electric_multirotor_plus_pusher,0.7980443671226225,0.9638764433470889,25.868645839210817,aluminum_lithium,medium_stiff,0.02,glass_composite,titanium,0.7,0.025659260822299933,1.3927642709063583,2.8436502337938294,1.1734017288870509,11.36099878290237,3.5012466571711194,4,65.77128776047441,3.2415769217822143,True,True,True,3.2415769217822143,"Bio-inspired by osprey, cheetah, harpy_eagle, tiger, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 15.5 kg, and carries a payload of 50.3 kg (3.24:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.6 kg battery (~1429 Wh usable) at about 84 V. Estimated battery peak power is ~9.8 kW. It also includes ~2.1 kg of supercapacitors (~82 Wh) that can provide high peak power (up to ~3.3 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~26 A. The main frame uses aluminum lithium (medium_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic mission model, it cruises at about 11.4 m/s and climbs at about 3.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.24. ",rotor_plus_pusher,multirotor,pusher_propeller,0.23213636236100876,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, cheetah, harpy_eagle, tiger, golden_eagle, with 8 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",1.0,1.0,0.0,1.0,5
+DLIFT_c1204acfb0,"harpy_eagle,dragonfly,tiger,bee","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,8,21.08781482900283,50.91526755554111,23,1.4446952402029245,1.7484282220831127,5.577279195225709,0.03459602147328525,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.904434449798168,259.39389958695887,2050.362075962644,46.112951370331416,17979.260635423907,1.331839304509474,53.27357218037896,2130.9428872151584,electric_multirotor_plus_micro_turbojet,0.7968344427595404,0.9619005888379555,25.637184000376703,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.7844504290739202,0.2222445314421477,1.2,2.946237850531656,2.0500777149931864,5.130339090464826,3.0543490119048866,5,72.00308238454394,2.4144401858800233,True,True,True,2.4144401858800233,"Bio-inspired by harpy_eagle, dragonfly, tiger, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 21.1 kg, and carries a payload of 50.9 kg (2.41:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.9 kg battery (~2050 Wh usable) at about 46 V. Estimated battery peak power is ~18.0 kW. It also includes ~1.3 kg of supercapacitors (~53 Wh) that can provide high peak power (up to ~2.1 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~26 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 5.1 m/s and climbs at about 3.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.41. ",rotor_plus_small_jet,multirotor,small_jet,0.2223409133175671,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, dragonfly, tiger, bee, with 23 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_87d4da3855,"bat,golden_eagle,albatross,harpy_eagle,tiger","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,10,17.476527371123645,51.38983098703437,9,1.7024154306380668,1.3447424007797355,19.179208681119512,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.539740387314511,239.34772701015547,1565.271996940242,49.352496825973034,7990.692997383812,2.3889052173759016,95.55620869503606,3822.2483478014424,electric_brushless_outunner,0.884629058879668,0.941290388749552,38.453624988632335,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.3830565140401835,0.25029838838819723,0.8530093520481854,1.9921940319253755,1.2643621302774384,21.684362037320412,5.171897642942561,5,68.86635835815801,2.9405058508331274,True,True,True,2.9405058508331274,"Bio-inspired by bat, golden_eagle, albatross, harpy_eagle, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 17.5 kg, and carries a payload of 51.4 kg (2.94:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.5 kg battery (~1565 Wh usable) at about 49 V. Estimated battery peak power is ~8.0 kW. It also includes ~2.4 kg of supercapacitors (~96 Wh) that can provide high peak power (up to ~3.8 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~38 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; reinforced landing gear designed to tolerate higher touchdown loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~4.9 s with a synthetic deployment failure risk of ~7.5%. In the synthetic mission model, it cruises at about 21.7 m/s and climbs at about 5.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.94. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,4.870296975760322,0.07466589589539503,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, golden_eagle, albatross, harpy_eagle, tiger, with 9 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.2,0.8,5
+DLIFT_11336b614f,bat,"WING_FOLDABLE,WING_MORPHING_MEMBRANE",1,2,21.42949108245284,75.23049197748504,11,1.8528111151639248,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.613818425560337,194.89886258303451,1678.823413638495,55.26397754297072,16771.01863414593,0.0,0.0,0.0,electric_brushless_outunner,0.826941373643088,0.9693232043514021,35.07679983072315,carbon_composite,light_stiff,0.01,carbon_composite,titanium,1.0581681355791042,0.0,1.3669315370719235,3.3689756848065806,2.305738669405987,9.813896163191254,4.272443516693661,6,96.65998305993789,3.510605626985057,True,True,True,3.510605626985057,"Bio-inspired by bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 21.4 kg, and carries a payload of 75.2 kg (3.51:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.6 kg battery (~1679 Wh usable) at about 55 V. Estimated battery peak power is ~16.8 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~35 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include foldable wings that deploy after vertical takeoff for cruise efficiency; morphing lifting surface that can change camber and area for control and efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.0 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 9.8 m/s and climbs at about 4.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.51. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,5.994876474506035,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, with 11 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.4,0.4,0.5,0.42000000000000004,3
+DLIFT_a01e869cc8,tiger,"LIFT_BURST_POWER,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",1,3,15.495293021647564,51.0105143680863,12,1.8444524005978273,2.9492948616026395,3.7483443405506605,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.784859335484873,220.80764245143632,2381.379364038779,36.58736473454783,27181.293765571525,0.7454810529846225,29.819242119384903,1192.7696847753962,electric_multirotor_plus_pusher,0.8694735832451966,0.9550961760611824,63.49850471948303,magnesium_alloy,very_light_fragile,0.04,aluminum,steel,0.8382872987704921,0.0902704052706952,1.2711758669371824,2.9530066736613985,2.263464121158214,7.274958905373349,2.8513557588115495,3,66.50580738973386,3.2920006286310626,True,True,True,3.2920006286310626,"Bio-inspired by tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 15.5 kg, and carries a payload of 51.0 kg (3.29:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.8 kg battery (~2381 Wh usable) at about 37 V. Estimated battery peak power is ~27.2 kW. It also includes ~0.7 kg of supercapacitors (~30 Wh) that can provide high peak power (up to ~1.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~63 A. The main frame uses magnesium alloy (very_light_fragile), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 7.3 m/s and climbs at about 2.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.29. ",rotor_plus_pusher,multirotor,pusher_propeller,0.2411282501547398,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, with 12 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_04bf6dc19d,"tiger,bee","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,5,22.44533730212926,72.84286586072272,20,1.9546274523480998,1.1036320677018623,17.170055274052416,0.23757266377002184,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.467044781867243,238.11871576660945,1301.8056824967716,91.53062343987196,5685.710955178172,1.3204270806275304,52.817083225101214,2112.6833290040486,electric_brushless_outunner,0.8834344895522022,0.9765670002130342,5.653970412238917,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.9772102090793493,0.558784258863025,0.7576274488187299,1.7635899182899706,2.9669361797679956,11.949109126356676,5.188434060009553,4,95.28820316285199,3.2453451191313816,True,True,True,3.2453451191313816,"Bio-inspired by tiger, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 22.4 kg, and carries a payload of 72.8 kg (3.25:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.5 kg battery (~1302 Wh usable) at about 92 V. Estimated battery peak power is ~5.7 kW. It also includes ~1.3 kg of supercapacitors (~53 Wh) that can provide high peak power (up to ~2.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~6 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 11.9 m/s and climbs at about 5.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.25. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, bee, with 20 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_e804778d35,"bee,harpy_eagle,dragonfly,tiger","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,8,13.315367298535358,76.45221343866481,15,2.042096046680957,2.6459203095266295,15.24902813633778,0.02092132519204734,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.655833181754566,187.78229267064057,1625.412199844478,66.53039395296247,6394.9770751666465,1.305846038756385,52.233841550255406,2089.3536620102163,electric_ducted_fan,0.8037293080775352,0.9518787035671994,14.844622649925338,carbon_composite,light_stiff,0.01,glass_composite,steel,0.4574729105931479,0.542144138926904,1.321964564850935,2.1861531915616013,2.2966011924165284,17.984663221121046,4.3365462880695835,6,89.76758073720018,5.741652612697682,True,True,True,5.741652612697682,"Bio-inspired by bee, harpy_eagle, dragonfly, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 13.3 kg, and carries a payload of 76.5 kg (5.74:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.7 kg battery (~1625 Wh usable) at about 67 V. Estimated battery peak power is ~6.4 kW. It also includes ~1.3 kg of supercapacitors (~52 Wh) that can provide high peak power (up to ~2.1 kW). The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~15 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 18.0 m/s and climbs at about 4.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.74. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, harpy_eagle, dragonfly, tiger, with 15 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_998ae2cbdf,"bee,tiger,dragonfly","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,6,12.981348944614671,79.2297176725913,17,1.919540477897193,1.8379957251910102,16.83855483380182,0.09073363206885776,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,7.038677175449972,390.7342649763179,2750.25235255503,94.62975495714657,12638.479196326944,0.9119212451936068,36.47684980774427,1459.0739923097708,electric_multirotor_plus_micro_turbojet,0.8823682347061103,0.9799710224614792,8.176158990358266,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.45667151916836696,0.4803277361693626,1.6612685384330588,2.4938407365017317,1.3366805079438935,18.49492364599584,2.7493170875417827,5,92.21106661720597,6.103350122597225,True,True,True,6.103350122597225,"Bio-inspired by bee, tiger, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 17 rotors, has an empty mass of 13.0 kg, and carries a payload of 79.2 kg (6.10:1 payload-to-aircraft mass ratio). The energy system is li-s with a 7.0 kg battery (~2750 Wh usable) at about 95 V. Estimated battery peak power is ~12.6 kW. It also includes ~0.9 kg of supercapacitors (~36 Wh) that can provide high peak power (up to ~1.5 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~8 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 18.5 m/s and climbs at about 2.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 6.10. ",rotor_plus_small_jet,multirotor,small_jet,0.2731455179322687,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, tiger, dragonfly, with 17 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_c812a2e7ae,tiger,"LIFT_BURST_POWER,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",1,3,17.274980353833286,51.337370466384364,5,1.3342246908382749,2.503503633826535,18.824374146356583,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.0533143567233925,234.34858314459245,1652.9342259715395,50.64953357710739,10851.833245232838,0.6372804158183364,25.491216632733455,1019.6486653093382,electric_multirotor_plus_pusher,0.9021889896089619,0.9757517274101634,27.5777270685463,steel_truss,heavy_robust,0.01,carbon_composite,composite,0.7025241134223029,0.35956146580426834,1.0346010928158327,3.041038925308894,2.7307485148220563,9.1204351538293,2.980390948788677,6,68.61235082021764,2.9717759102975014,True,True,True,2.9717759102975014,"Bio-inspired by tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 17.3 kg, and carries a payload of 51.3 kg (2.97:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.1 kg battery (~1653 Wh usable) at about 51 V. Estimated battery peak power is ~10.9 kW. It also includes ~0.6 kg of supercapacitors (~25 Wh) that can provide high peak power (up to ~1.0 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~28 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 9.1 m/s and climbs at about 3.0 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.97. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5987649405526156,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, with 5 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_b443e4addf,"harpy_eagle,bee,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,6,20.872502588496047,73.18438195215353,23,2.479265021630005,1.7945585992083828,14.995526917091937,0.19141144740076582,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,3.02559530734694,375.68608646084823,1136.6740602314792,86.54436077916307,4323.824730129485,0.04046157122540872,1.6184628490163488,64.73851396065396,electric_brushless_outunner,0.8008959919528356,0.9409287587194769,2.936571957428123,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.5943564875800265,0.0,1.3113959415942809,0.5578877888705773,0.5011567365880623,21.777419873311757,5.350459270356513,4,94.05688454064958,3.5062581327688687,True,True,True,3.5062581327688687,"Bio-inspired by harpy_eagle, bee, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 20.9 kg, and carries a payload of 73.2 kg (3.51:1 payload-to-aircraft mass ratio). The energy system is li-s with a 3.0 kg battery (~1137 Wh usable) at about 87 V. Estimated battery peak power is ~4.3 kW. It also includes ~0.0 kg of supercapacitors (~2 Wh) that can provide high peak power (up to ~0.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~3 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 21.8 m/s and climbs at about 5.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.51. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, bee, dragonfly, with 23 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_c05972a18e,harpy_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,13.01448602749144,58.4597081389451,9,1.233485495920259,1.3274741662157874,15.620893555851534,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.071553320291909,227.95086193271646,928.1140887655542,74.65808625457544,5775.489983714447,2.7948485265248038,111.79394106099215,4471.757642439687,electric_multirotor_plus_micro_turbojet,0.8929235365693492,0.9650149569802261,17.268950484608805,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.7880568887314385,0.0,1.9020708907583739,1.778985024938905,1.8913255425749802,9.409518176175682,4.839772346550035,4,71.47419416643655,4.491895263128827,True,True,True,4.491895263128827,"Bio-inspired by harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 13.0 kg, and carries a payload of 58.5 kg (4.49:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.1 kg battery (~928 Wh usable) at about 75 V. Estimated battery peak power is ~5.8 kW. It also includes ~2.8 kg of supercapacitors (~112 Wh) that can provide high peak power (up to ~4.5 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~17 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 9.4 m/s and climbs at about 4.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.49. ",rotor_plus_small_jet,multirotor,small_jet,0.2732695995584433,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, with 9 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.3,0.3,0.7,0.30000000000000004,3
+DLIFT_859f6f2967,"dragonfly,tiger,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,7,17.02499866896543,79.55789635655125,15,2.0308827021271125,1.746591948557886,11.230839700681281,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.267630511925949,218.71306040927536,714.6734695500514,28.80058882963494,2642.1881116060704,2.043997644743642,81.75990578974569,3270.3962315898275,electric_brushless_outunner,0.9060153643936542,0.9543310228764352,17.329954474001468,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.9886913319681778,0.38065742834171845,1.9294556682923067,1.8177133319279726,2.7064910546431196,10.427736837179273,2.3697136708948037,3,96.58289502551668,4.673004556621549,True,True,True,4.673004556621549,"Bio-inspired by dragonfly, tiger, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 17.0 kg, and carries a payload of 79.6 kg (4.67:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.3 kg battery (~715 Wh usable) at about 29 V. Estimated battery peak power is ~2.6 kW. It also includes ~2.0 kg of supercapacitors (~82 Wh) that can provide high peak power (up to ~3.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~17 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads. In the synthetic mission model, it cruises at about 10.4 m/s and climbs at about 2.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.67. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, tiger, golden_eagle, with 15 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_55755f8de9,"harpy_eagle,cheetah,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",3,8,14.155421344743976,78.3407434099829,22,1.7419753349839695,1.6340162265290112,13.208055716875524,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.704110273552805,249.70819855039085,2672.9040934936024,69.45235411353914,13749.355815861496,0.9658264036096745,38.633056144386984,1545.3222457754794,electric_multirotor_plus_pusher,0.8824693591484539,0.9673505294404429,8.539339473082835,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.7,0.12798930247731607,1.2,3.070117643733271,2.457944701602162,14.282444372588184,4.083169741257061,4,92.49616475472688,5.534327908866624,True,True,True,5.534327908866624,"Bio-inspired by harpy_eagle, cheetah, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 14.2 kg, and carries a payload of 78.3 kg (5.53:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.7 kg battery (~2673 Wh usable) at about 69 V. Estimated battery peak power is ~13.7 kW. It also includes ~1.0 kg of supercapacitors (~39 Wh) that can provide high peak power (up to ~1.5 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~9 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy. In the synthetic mission model, it cruises at about 14.3 m/s and climbs at about 4.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.53. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4914284956444841,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, cheetah, dragonfly, with 22 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.3,0.3,0.7,0.30000000000000004,3
+DLIFT_5fb6eeb234,"bee,dragonfly,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,6,23.536621537495243,50.78564930115568,12,1.6404441545907387,1.0378632785210395,8.028201828958556,0.18810693143250104,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.475168282771066,204.02272450399846,709.0133011608347,28.60190395222914,6119.209720700979,0.08281829686793996,3.3127318747175982,132.50927498870394,electric_brushless_outunner,0.8696651352127022,0.9821841707854707,22.050995073446938,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.7244625567356551,0.0,1.8491631523104757,1.4823449910227642,0.5738727005368696,17.720179663437293,3.4228680486585326,4,74.32227083865092,2.1577289340465073,True,True,True,2.1577289340465073,"Bio-inspired by bee, dragonfly, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 23.5 kg, and carries a payload of 50.8 kg (2.16:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.5 kg battery (~709 Wh usable) at about 29 V. Estimated battery peak power is ~6.1 kW. It also includes ~0.1 kg of supercapacitors (~3 Wh) that can provide high peak power (up to ~0.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~22 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 17.7 m/s and climbs at about 3.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.16. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, dragonfly, golden_eagle, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.2,0.2,0.8,0.2,3
+DLIFT_2c225ee5da,"harpy_eagle,cheetah,tiger,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,9,20.70237425886173,72.19173812215726,9,1.9530159418506825,2.3386175135388783,4.445584902000106,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.102611307620274,256.1311608907404,2331.462401357961,84.81140358528312,9661.920295957156,1.2645812633707223,50.58325053482889,2023.3300213931557,electric_multirotor_plus_pusher,0.8068739512572708,0.9466540844446246,11.550976588776994,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.7,0.5472396655695705,1.2800053609372641,2.1432369142312573,1.649110433896722,19.892243599006036,2.6578139135001293,5,92.894112381019,3.4871236129476944,True,True,True,3.4871236129476944,"Bio-inspired by harpy_eagle, cheetah, tiger, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 20.7 kg, and carries a payload of 72.2 kg (3.49:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.1 kg battery (~2331 Wh usable) at about 85 V. Estimated battery peak power is ~9.7 kW. It also includes ~1.3 kg of supercapacitors (~51 Wh) that can provide high peak power (up to ~2.0 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~12 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; reinforced landing gear designed to tolerate higher touchdown loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.6 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 19.9 m/s and climbs at about 2.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.49. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5004858504233562,1.05,0.9,0.01,True,2.559061579110412,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, cheetah, tiger, bat, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.5,0.5,0.4,0.52,3
+DLIFT_5addf9ea06,"albatross,dragonfly","LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_HIGH_ASPECT",2,5,18.507508142626538,78.21781997094473,12,1.300815464136048,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.375725334185552,253.99431073938237,1873.39227245946,92.81506278273079,20901.899174643288,0.0,0.0,0.0,electric_brushless_outunner,0.8956778936925479,0.9770570942831419,24.393995522869723,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.5024728274138937,0.0,1.2,1.133264521568792,0.5201836719528194,24.047915451564116,4.43158751923015,2,96.72532811357127,4.2262750537871305,True,True,True,4.2262750537871305,"Bio-inspired by albatross, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 18.5 kg, and carries a payload of 78.2 kg (4.23:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.4 kg battery (~1873 Wh usable) at about 93 V. Estimated battery peak power is ~20.9 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~24 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic mission model, it cruises at about 24.0 m/s and climbs at about 4.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.23. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, dragonfly, with 12 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.2,0.2,0.7,0.22000000000000003,3
+DLIFT_c14734722e,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,21.67105503616859,71.59060723469011,10,1.451323517898616,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.966251034022719,249.1508601977253,2483.10001807323,33.89145135675375,21534.419753676437,0.0,0.0,0.0,electric_brushless_outunner,0.8118827671800436,0.9587043788680832,84.1064821774121,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.3627238212376574,0.0,1.2,1.701461902216391,1.1409627899970576,10.911388003651961,2.9461965331017557,4,93.2616622708587,3.3035127784598726,True,True,True,3.3035127784598726,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 21.7 kg, and carries a payload of 71.6 kg (3.30:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.0 kg battery (~2483 Wh usable) at about 34 V. Estimated battery peak power is ~21.5 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~84 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 10.9 m/s and climbs at about 2.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.30. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 10 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.9,0.9,0.1,0.9000000000000001,5
+DLIFT_9307b335ad,osprey,"PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",1,3,21.871882415497883,67.40292345207082,6,2.298481721477015,1.0,0.0,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,8.418973307957021,302.9472843871887,2550.5051009738063,42.232815843177626,8904.247610537326,0.0,0.0,0.0,electric_brushless_outunner,0.8804760091973521,0.9509060050801132,48.34165054082706,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.9152078715062117,0.0,1.6121983539583913,2.958846992695882,0.6054688313265333,11.787390710688165,2.682368844019993,5,89.2748058675687,3.0817157010825347,True,True,True,3.0817157010825347,"Bio-inspired by osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 21.9 kg, and carries a payload of 67.4 kg (3.08:1 payload-to-aircraft mass ratio). The energy system is li-s with a 8.4 kg battery (~2551 Wh usable) at about 42 V. Estimated battery peak power is ~8.9 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~48 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 11.8 m/s and climbs at about 2.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.08. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, with 6 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.4,0.4,0.6,0.4,3
+DLIFT_de8d1ebdab,albatross,"LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_HIGH_ASPECT",1,3,22.57687421643473,72.11689567360253,10,1.9594338190955536,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.374116126869634,238.67361383467838,1282.6597171672004,64.53113430748866,8047.583118799939,0.0,0.0,0.0,electric_brushless_outunner,0.8756903708837044,0.9476945500884641,20.614563205681513,titanium_alloy,heavy_robust,0.005,carbon_composite,steel,0.5107862533127505,0.0,0.8117550540446501,2.994321795191857,2.1485360046870454,13.66506037872172,4.718352766577132,6,94.69376989003726,3.194281678776656,True,True,True,3.194281678776656,"Bio-inspired by albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 22.6 kg, and carries a payload of 72.1 kg (3.19:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.4 kg battery (~1283 Wh usable) at about 65 V. Estimated battery peak power is ~8.0 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~21 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic mission model, it cruises at about 13.7 m/s and climbs at about 4.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.19. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, with 10 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_7a4e0e501a,"albatross,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",2,7,15.255671399433187,62.622661029173464,5,1.6120092496384841,1.159254486308371,4.169801087891879,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.683607271081093,254.87609387663386,1448.6156203819835,29.01935330892803,4600.9385920343375,1.9560318366941472,78.2412734677659,3129.6509387106357,electric_multirotor_plus_pusher,0.9024625529781176,0.9721527510951389,64.76560485710931,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.7,0.4723097800073373,1.706997727433317,2.6626717537257933,1.5032796181482804,18.112308743196692,5.413936586942254,4,77.87833242860665,4.1048774183416255,True,True,True,4.1048774183416255,"Bio-inspired by albatross, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 15.3 kg, and carries a payload of 62.6 kg (4.10:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.7 kg battery (~1449 Wh usable) at about 29 V. Estimated battery peak power is ~4.6 kW. It also includes ~2.0 kg of supercapacitors (~78 Wh) that can provide high peak power (up to ~3.1 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~65 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 18.1 m/s and climbs at about 5.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.10. ",rotor_plus_pusher,multirotor,pusher_propeller,0.32391249640796393,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, cheetah, with 5 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.1,0.1,0.9,0.1,3
+DLIFT_c6bfcb4a4f,"golden_eagle,bat,albatross,bee,tiger","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,12,21.31439187110996,53.65675425748597,18,1.3470181889491415,1.1581544509856605,7.601432857678318,0.0965137139505598,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,11.385723396322861,317.39794914343145,3613.805255507261,62.2558252200687,15216.299356701584,0.9903734460451332,39.61493784180533,1584.5975136722132,electric_multirotor_plus_pusher,0.837624647558235,0.9407925494173563,14.637204004877875,carbon_composite,light_stiff,0.01,glass_composite,composite,0.7435553864868785,0.07889025231077497,1.017371884381229,2.327560720035968,3.4944614181577265,24.112181935396368,4.880462543443613,5,74.97114612859593,2.51739550356178,True,True,True,2.51739550356178,"Bio-inspired by golden_eagle, bat, albatross, bee, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 21.3 kg, and carries a payload of 53.7 kg (2.52:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 11.4 kg battery (~3614 Wh usable) at about 62 V. Estimated battery peak power is ~15.2 kW. It also includes ~1.0 kg of supercapacitors (~40 Wh) that can provide high peak power (up to ~1.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~15 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity. It uses foldable wings that deploy after takeoff. The wing deployment time is ~3.2 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 24.1 m/s and climbs at about 4.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.52. ",rotor_plus_pusher,multirotor,pusher_propeller,0.38289682262030234,1.05,0.9,0.01,True,3.2059034279149907,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, bat, albatross, bee, tiger, with 18 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged composite landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.1,0.66,4
+DLIFT_7b138b30c9,"cheetah,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",2,6,12.054388109261337,60.8738543105726,5,1.199327258125659,1.9719378322350682,11.658876171220436,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.977377315931957,240.01335011806663,954.6236542804329,93.3479521790448,5405.306276530507,1.4207110291893463,56.82844116757386,2273.137646702954,electric_brushless_outunner,0.8575712010651925,0.9817586568278761,21.54221866159016,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.7,0.49539799156356096,1.8172751566934089,0.7474959011601738,0.7892261629025796,22.47347820812701,5.37684774063179,4,72.92824241983394,5.0499331661474764,True,True,True,5.0499331661474764,"Bio-inspired by cheetah, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 12.1 kg, and carries a payload of 60.9 kg (5.05:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.0 kg battery (~955 Wh usable) at about 93 V. Estimated battery peak power is ~5.4 kW. It also includes ~1.4 kg of supercapacitors (~57 Wh) that can provide high peak power (up to ~2.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~22 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 22.5 m/s and climbs at about 5.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.05. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, golden_eagle, with 5 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_343743534c,"golden_eagle,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",2,3,13.778014069804733,66.43947929004514,6,1.7727960270108725,1.112077713199969,3.300573568186638,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.7202863288999355,186.17378198977414,1437.3149038952504,85.60258836106733,16875.1160562542,1.5717994779097948,62.87197911639179,2514.8791646556715,electric_multirotor_plus_pusher,0.8234951777890621,0.9627893008932927,50.84303401954726,carbon_composite,light_stiff,0.01,glass_composite,steel,0.6372283157205222,0.0,1.5495066261348553,1.1615020879632731,1.24739239863901,22.944295831065915,2.150770584474448,2,80.21749335984987,4.822137570294029,True,True,True,4.822137570294029,"Bio-inspired by golden_eagle, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 13.8 kg, and carries a payload of 66.4 kg (4.82:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.7 kg battery (~1437 Wh usable) at about 86 V. Estimated battery peak power is ~16.9 kW. It also includes ~1.6 kg of supercapacitors (~63 Wh) that can provide high peak power (up to ~2.5 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~51 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 22.9 m/s and climbs at about 2.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.82. ",rotor_plus_pusher,multirotor,pusher_propeller,0.21591676342993013,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, harpy_eagle, with 6 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_3c288d9170,"tiger,bee,osprey","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,8,15.523975945933437,55.25719179117585,12,1.868693873707081,2.570651909369589,7.000446634937118,0.17905066220411914,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,3.538864028640878,276.8111493481049,979.5970191547462,75.3860768086342,8873.360350550929,0.39366355682500553,15.746542273000221,629.8616909200089,electric_multirotor_plus_pusher,0.8677637545135513,0.9639427853067072,12.637883616986151,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.5499352026410325,0.21967918673047884,1.572422612345516,3.0638065069791938,1.6024232374967715,7.802925331146597,4.680879979895999,5,70.78116773710929,3.5594741955040634,True,True,True,3.5594741955040634,"Bio-inspired by tiger, bee, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 15.5 kg, and carries a payload of 55.3 kg (3.56:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 3.5 kg battery (~980 Wh usable) at about 75 V. Estimated battery peak power is ~8.9 kW. It also includes ~0.4 kg of supercapacitors (~16 Wh) that can provide high peak power (up to ~0.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~13 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 7.8 m/s and climbs at about 4.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.56. ",rotor_plus_pusher,multirotor,pusher_propeller,0.29718373942675347,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, bee, osprey, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_2298611994,"cheetah,bat,tiger","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,7,22.96595682270225,75.7844436194758,5,1.11824187386654,1.5674193512206045,12.313243553231883,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,5.354857711649389,273.1674614976195,1462.7728877722154,55.489911819816754,11145.508857467245,0.26583468135099975,10.63338725403999,425.3354901615996,electric_ducted_fan,0.818122287132174,0.9744354020224061,65.16176344391295,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.38253455724351376,0.3100491243188293,0.7587621016838626,1.6370955790984858,2.8763243930643254,18.945198501198988,5.743757878892325,6,98.75040044217805,3.2998600582825075,True,True,True,3.2998600582825075,"Bio-inspired by cheetah, bat, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 23.0 kg, and carries a payload of 75.8 kg (3.30:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 5.4 kg battery (~1463 Wh usable) at about 55 V. Estimated battery peak power is ~11.1 kW. It also includes ~0.3 kg of supercapacitors (~11 Wh) that can provide high peak power (up to ~0.4 kW). The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~65 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.0 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 18.9 m/s and climbs at about 5.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.30. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,True,5.98908901452633,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, bat, tiger, with 5 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_cf9c52144e,"albatross,harpy_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,WING_HIGH_ASPECT",2,6,12.846644852487223,73.2662039462574,11,1.6522203687734736,1.630979976604889,5.636417140386088,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.482903573292234,245.12857908477795,2569.6592576038665,71.37420578721137,27658.04815561951,2.082637480441406,83.30549921765623,3332.2199687062493,electric_brushless_outunner,0.8749996268733289,0.9729286233396313,50.471672836994536,carbon_composite,light_stiff,0.01,carbon_composite,titanium,1.0011337254011294,0.0,1.4935425718013788,1.9114245264995473,1.9243505737874647,12.698128656964752,4.7992286840961444,2,86.11284879874464,5.703139207749829,True,True,True,5.703139207749829,"Bio-inspired by albatross, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 12.8 kg, and carries a payload of 73.3 kg (5.70:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.5 kg battery (~2570 Wh usable) at about 71 V. Estimated battery peak power is ~27.7 kW. It also includes ~2.1 kg of supercapacitors (~83 Wh) that can provide high peak power (up to ~3.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~50 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic mission model, it cruises at about 12.7 m/s and climbs at about 4.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.70. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, harpy_eagle, with 11 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.5,0.5,0.5,0.5,3
+DLIFT_fb373be4ff,"cheetah,golden_eagle,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,8,18.386163301123087,79.21299640801547,9,1.4466771952564188,1.0304114693413375,7.89766364286254,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.81821422489417,212.60039118036062,1874.7557937247211,24.14985390850859,14474.596645141228,0.5734952635742182,22.93981054296873,917.5924217187492,electric_multirotor_plus_micro_turbojet,0.7877654642033486,0.9536681144302848,87.7813361557102,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.5632524367428544,0.3364586443271894,0.6832843022785986,3.442197038851424,1.5269467801690981,19.03014204493182,2.5124707440963734,4,97.59915970913856,4.308293965994356,True,True,True,4.308293965994356,"Bio-inspired by cheetah, golden_eagle, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 18.4 kg, and carries a payload of 79.2 kg (4.31:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.8 kg battery (~1875 Wh usable) at about 24 V. Estimated battery peak power is ~14.5 kW. It also includes ~0.6 kg of supercapacitors (~23 Wh) that can provide high peak power (up to ~0.9 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~88 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. It uses foldable wings that deploy after takeoff. The wing deployment time is ~3.9 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 19.0 m/s and climbs at about 2.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.31. ",rotor_plus_small_jet,multirotor,small_jet,0.1865032601048297,1.15,0.85,0.03,True,3.8948122805517134,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, golden_eagle, bat, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_d9a8a5efa5,"harpy_eagle,bee,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,6,16.25478949352026,66.81984937942322,15,1.8046059020907141,1.759179382969542,4.6483099266784365,0.02821999957740498,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.413267722176599,247.7811507272973,2332.430308305042,84.20295311302351,8197.312204327929,2.3796495632020487,95.18598252808195,3807.439301123278,electric_brushless_outunner,0.8337991193362312,0.9804059020317104,16.463791466470752,steel_truss,heavy_robust,0.01,glass_composite,steel,0.6801990091016802,0.0,1.2,4.477039089361593,1.9202740586600318,23.821641152078353,3.2362402016775524,3,83.07463887294348,4.110779127964714,True,True,True,4.110779127964714,"Bio-inspired by harpy_eagle, bee, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 16.3 kg, and carries a payload of 66.8 kg (4.11:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.4 kg battery (~2332 Wh usable) at about 84 V. Estimated battery peak power is ~8.2 kW. It also includes ~2.4 kg of supercapacitors (~95 Wh) that can provide high peak power (up to ~3.8 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~16 A. The main frame uses steel truss (heavy_robust), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 23.8 m/s and climbs at about 3.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.11. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, bee, dragonfly, with 15 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.9,0.9,0.0,0.92,5
+DLIFT_6838f89ad6,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,15.96626493996282,79.75220104281185,9,1.3276915720167728,2.252581180876547,9.71878188327321,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.7367835808905516,251.14372513302473,938.4697485207765,90.71995826670842,4143.390001791761,0.7752651427453505,31.010605709814023,1240.424228392561,electric_brushless_outunner,0.8007721032915175,0.9747879092026052,9.971445516921557,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.36579601822754415,0.6557336060621521,1.5272084065701255,2.9323712917953437,1.4296292847164649,20.035562020601887,5.507005371395476,4,95.71846598277466,4.995044322682871,True,True,True,4.995044322682871,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 16.0 kg, and carries a payload of 79.8 kg (5.00:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.7 kg battery (~938 Wh usable) at about 91 V. Estimated battery peak power is ~4.1 kW. It also includes ~0.8 kg of supercapacitors (~31 Wh) that can provide high peak power (up to ~1.2 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~10 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 20.0 m/s and climbs at about 5.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.00. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_60041b0b5b,"albatross,osprey,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,10,21.109165506956785,77.54794631929775,12,2.4854201836380048,2.550809637327599,17.708041402499173,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.9390763953324575,257.6777086897895,2045.7230146624609,43.03603848317398,12096.65231904537,2.8468137237120645,113.87254894848257,4554.9019579393025,electric_brushless_outunner,0.8749614606706002,0.9591213736841478,46.07796413604908,magnesium_alloy,very_light_fragile,0.04,glass_composite,titanium,0.5073148000752895,0.06309040830856101,1.8449997791405526,1.659270298333987,1.7102107120037926,14.915083926969455,4.529833743538433,4,98.65711182625454,3.6736623384633975,True,True,True,3.6736623384633975,"Bio-inspired by albatross, osprey, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 21.1 kg, and carries a payload of 77.5 kg (3.67:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.9 kg battery (~2046 Wh usable) at about 43 V. Estimated battery peak power is ~12.1 kW. It also includes ~2.8 kg of supercapacitors (~114 Wh) that can provide high peak power (up to ~4.6 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~46 A. The main frame uses magnesium alloy (very_light_fragile), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; multiple flight modes to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic mission model, it cruises at about 14.9 m/s and climbs at about 4.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.67. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, osprey, cheetah, with 12 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_09f78c48fd,"bat,bee,cheetah,dragonfly,tiger","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,10,21.616090655522125,54.355346733869546,18,1.2953918609992303,1.2800322837218625,8.151037365231023,0.2482753278407016,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.1354940385123458,218.25992874780667,684.3527054348772,82.24215848177619,2415.306079681716,0.4784891591494047,19.139566365976187,765.5826546390474,electric_brushless_outunner,0.8430369907693198,0.9467595597456252,3.665854867344746,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.7,0.6806674670525478,1.2,4.421887776521014,2.6266939803889673,23.778080029093772,5.119696192740621,4,75.97143738939167,2.514578033562407,True,True,True,2.514578033562407,"Bio-inspired by bat, bee, cheetah, dragonfly, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 21.6 kg, and carries a payload of 54.4 kg (2.51:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.1 kg battery (~684 Wh usable) at about 82 V. Estimated battery peak power is ~2.4 kW. It also includes ~0.5 kg of supercapacitors (~19 Wh) that can provide high peak power (up to ~0.8 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~4 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.7 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 23.8 m/s and climbs at about 5.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.51. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,6.726782470388342,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, bee, cheetah, dragonfly, tiger, with 18 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_0bc55fb355,"albatross,bee","LIFT_ENERGY_DENSE,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,STAB_DISTRIBUTED_THRUST,WING_HIGH_ASPECT",2,5,18.40754690065511,74.76181459169052,15,2.0330254735035993,1.0,0.0,0.19151908557117445,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,10.465356245288515,335.42368906714216,3510.328399196529,58.32708714177405,9756.459049675992,0.0,0.0,0.0,electric_brushless_outunner,0.8262933316796295,0.9435683637909386,15.061471492425447,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.8654283438569956,0.0,1.2226234764079091,0.6207855836414966,0.5150304137162014,10.413486248534927,3.5264273055164654,3,93.16936149234563,4.0614762518426515,True,True,True,4.0614762518426515,"Bio-inspired by albatross, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 18.4 kg, and carries a payload of 74.8 kg (4.06:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 10.5 kg battery (~3510 Wh usable) at about 58 V. Estimated battery peak power is ~9.8 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~15 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; many smaller rotors for fine-grained control and redundancy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic mission model, it cruises at about 10.4 m/s and climbs at about 3.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.06. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, bee, with 15 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.3,0.3,0.5,0.34,3
+DLIFT_70a33a3128,"tiger,osprey,dragonfly,bee","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,8,15.135608976854318,74.67729613672688,10,1.8410958818029006,1.0656643947692255,4.96631079832903,0.0861159625500609,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.988681367569192,197.82075774013063,1580.3270014770005,62.661444834130236,15052.844540048298,1.2058404447798758,48.23361779119503,1929.3447116478012,electric_multirotor_plus_pusher,0.8516441905731592,0.945403679294421,31.104687631735693,magnesium_alloy,very_light_fragile,0.04,carbon_composite,titanium,0.6233571174026092,0.5429345336755057,1.2,2.5581798710331234,1.8512231022023014,16.752846443212455,3.488543577297708,5,89.8129051135812,4.933881170617246,True,True,True,4.933881170617246,"Bio-inspired by tiger, osprey, dragonfly, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 15.1 kg, and carries a payload of 74.7 kg (4.93:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.0 kg battery (~1580 Wh usable) at about 63 V. Estimated battery peak power is ~15.1 kW. It also includes ~1.2 kg of supercapacitors (~48 Wh) that can provide high peak power (up to ~1.9 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~31 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 16.8 m/s and climbs at about 3.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.93. ",rotor_plus_pusher,multirotor,pusher_propeller,0.24493639512382331,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, dragonfly, bee, with 10 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.2,0.72,4
+DLIFT_3400d75369,"bat,osprey","PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,5,15.400945928290492,64.84840724558111,8,2.245368691488572,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.240092742515255,255.74002765884947,2107.321545882336,64.20126808856915,23693.458220115004,0.0,0.0,0.0,electric_brushless_outunner,0.8500819367444755,0.9648901895967014,63.775409530027375,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.35900593674188136,0.0,1.2890124379910992,2.197521353488836,2.0600948196523072,15.80764471069818,3.0995502146664933,6,80.24935317387161,4.210676899167537,True,True,True,4.210676899167537,"Bio-inspired by bat, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 15.4 kg, and carries a payload of 64.8 kg (4.21:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.2 kg battery (~2107 Wh usable) at about 64 V. Estimated battery peak power is ~23.7 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~64 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency; morphing lifting surface that can change camber and area for control and efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.0 s with a synthetic deployment failure risk of ~9.9%. In the synthetic mission model, it cruises at about 15.8 m/s and climbs at about 3.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.21. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,6.017555689176466,0.09895671626801236,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, osprey, with 8 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.3,0.62,4
+DLIFT_9e1a2aaf12,"osprey,albatross,golden_eagle,dragonfly","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_HIGH_ASPECT",4,10,20.09145029100649,71.24935317428849,10,1.3131684478052383,2.0418228862513264,18.623580138188814,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.583173984491851,253.8235141699984,1924.7878693062305,26.425631368436903,8011.166735057539,0.7504225464992419,30.016901859969675,1200.676074398787,electric_brushless_outunner,0.8145120836248246,0.9751944100693006,51.24585157539962,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.8927615414195605,0.0,1.9207058675486741,2.9110341042802554,0.656286915724795,5.096068643277807,4.7959420077127906,6,91.34080346529498,3.546252368161882,True,True,True,3.546252368161882,"Bio-inspired by osprey, albatross, golden_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 20.1 kg, and carries a payload of 71.2 kg (3.55:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.6 kg battery (~1925 Wh usable) at about 26 V. Estimated battery peak power is ~8.0 kW. It also includes ~0.8 kg of supercapacitors (~30 Wh) that can provide high peak power (up to ~1.2 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~51 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight. In the synthetic mission model, it cruises at about 5.1 m/s and climbs at about 4.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.55. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, albatross, golden_eagle, dragonfly, with 10 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_cf52825e39,"cheetah,tiger","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,5,15.533566138842566,73.96806293457186,9,1.4774434489096109,2.596637279990196,7.163177894226213,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.4690326332348325,245.99387490250405,853.3607796126736,71.66059954950958,9542.057396904362,1.4967525795181051,59.87010318072421,2394.8041272289684,electric_multirotor_plus_micro_turbojet,0.849997204793959,0.9575964250204098,27.206143268209818,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.7,0.35545055983761814,1.4688918928624537,2.54725634164428,2.222776208761538,11.304636340548363,2.6220013224957,6,89.50162907341442,4.761821095904726,True,True,True,4.761821095904726,"Bio-inspired by cheetah, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 15.5 kg, and carries a payload of 74.0 kg (4.76:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.5 kg battery (~853 Wh usable) at about 72 V. Estimated battery peak power is ~9.5 kW. It also includes ~1.5 kg of supercapacitors (~60 Wh) that can provide high peak power (up to ~2.4 kW). The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~27 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 11.3 m/s and climbs at about 2.6 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.76. ",rotor_plus_small_jet,multirotor,small_jet,0.18006408155810333,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, tiger, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_0f915f2faf,"harpy_eagle,albatross,bee","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,WING_HIGH_ASPECT",3,8,14.07788799026699,74.12196063261516,8,1.5082028644925505,1.234200288179476,8.324063217043427,0.16978234365033945,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.939888525699349,226.8662231263656,2708.757414375241,81.65689891149313,17835.29270330491,2.0839504513746943,83.35801805498777,3334.320722199511,electric_brushless_outunner,0.8845887632586855,0.9649979544165165,46.06225468071274,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.5166548779703564,0.0,0.8342702765335785,2.5611970805192774,1.5492575815449166,18.769108390972242,5.484632940887721,2,88.19984862288214,5.265133568604947,True,True,True,5.265133568604947,"Bio-inspired by harpy_eagle, albatross, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 14.1 kg, and carries a payload of 74.1 kg (5.27:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.9 kg battery (~2709 Wh usable) at about 82 V. Estimated battery peak power is ~17.8 kW. It also includes ~2.1 kg of supercapacitors (~83 Wh) that can provide high peak power (up to ~3.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~46 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 18.8 m/s and climbs at about 5.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.27. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, albatross, bee, with 8 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.1,0.74,4
+DLIFT_b1d3232110,"albatross,bat,dragonfly,bee,harpy_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,11,22.921011650737462,64.27327863836263,24,2.319729595457372,2.160101999995099,13.035839436893369,0.2380291278696321,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.064144717307844,225.19462063953213,1365.6127691173629,91.27329687194357,6238.867172741603,1.32460694885485,52.984277954194,2119.37111816776,electric_brushless_outunner,0.8910061883459612,0.9821037903647455,5.59132945867608,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.6659741683282434,0.0,1.2,2.2893134749958888,1.3111232324146804,19.600246720901893,5.277809543490032,3,87.19429028910008,2.8041204994673388,True,True,True,2.8041204994673388,"Bio-inspired by albatross, bat, dragonfly, bee, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 24 rotors, has an empty mass of 22.9 kg, and carries a payload of 64.3 kg (2.80:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.1 kg battery (~1366 Wh usable) at about 91 V. Estimated battery peak power is ~6.2 kW. It also includes ~1.3 kg of supercapacitors (~53 Wh) that can provide high peak power (up to ~2.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~6 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity. It uses foldable wings that deploy after takeoff. The wing deployment time is ~4.1 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 19.6 m/s and climbs at about 5.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.80. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,4.096342048536697,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, bat, dragonfly, bee, harpy_eagle, with 24 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_dbba0b6e5b,"tiger,osprey","LIFT_BURST_POWER,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,6,19.187964472465996,67.41853753010267,12,1.3828162705493043,1.794422932782359,16.664904244071344,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.542934118861481,193.48569829023472,2233.392668306089,25.517555358251947,17748.157056122807,0.9139034555423952,36.556138221695804,1462.245528867832,electric_brushless_outunner,0.8502539667374597,0.9789828831412771,93.93063227423005,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.986824909610402,0.25413709144634666,1.2,3.6610926319957198,3.596100326095069,8.675767383302308,3.6724993254967995,6,86.60650200256866,3.5135846549458503,True,True,True,3.5135846549458503,"Bio-inspired by tiger, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 19.2 kg, and carries a payload of 67.4 kg (3.51:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.5 kg battery (~2233 Wh usable) at about 26 V. Estimated battery peak power is ~17.7 kW. It also includes ~0.9 kg of supercapacitors (~37 Wh) that can provide high peak power (up to ~1.5 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~94 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 8.7 m/s and climbs at about 3.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.51. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, with 12 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.5,0.5,0.5,0.5,3
+DLIFT_3bc0e4754b,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,13.557874453519277,79.67930215848638,4,1.8589657726341318,1.6924752926512534,7.532166014148277,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.33485914557022,183.97085248960437,1349.4002899017244,63.16031055782944,15650.826786311778,1.7832228462360384,71.32891384944153,2853.156553977661,electric_brushless_outunner,0.8326949366566424,0.9822749899857586,116.15103924020497,carbon_composite,light_stiff,0.01,aluminum,composite,0.7,0.5258372772069552,1.402210161926493,3.2945040625048736,2.1975247863587244,10.62530556748284,5.730551014412825,4,93.23717661200565,5.87697595457551,True,True,True,5.87697595457551,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 13.6 kg, and carries a payload of 79.7 kg (5.88:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.3 kg battery (~1349 Wh usable) at about 63 V. Estimated battery peak power is ~15.7 kW. It also includes ~1.8 kg of supercapacitors (~71 Wh) that can provide high peak power (up to ~2.9 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~116 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 10.6 m/s and climbs at about 5.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.88. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 4 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.3,0.62,4
+DLIFT_c978c035ed,"bee,harpy_eagle,tiger,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,9,23.53924359151911,51.61362280382642,10,2.0860569065504073,2.1781723877988606,6.694402619256515,0.10747219227482357,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.998017759359634,199.10336104562543,1990.6389396823563,28.298494680294986,22361.90785233389,2.220369322497443,88.81477289989772,3552.5909159959087,electric_brushless_outunner,0.8980234462294013,0.9468059166525401,137.5758924017752,aluminum_lithium,medium_stiff,0.02,glass_composite,steel,0.44761178532823165,0.2742358786844464,1.6472469766901296,1.3492246830505181,3.2802869092505746,21.925763253504854,4.346690162322785,6,75.15286639534554,2.1926627592410046,True,True,True,2.1926627592410046,"Bio-inspired by bee, harpy_eagle, tiger, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 23.5 kg, and carries a payload of 51.6 kg (2.19:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.0 kg battery (~1991 Wh usable) at about 28 V. Estimated battery peak power is ~22.4 kW. It also includes ~2.2 kg of supercapacitors (~89 Wh) that can provide high peak power (up to ~3.6 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~138 A. The main frame uses aluminum lithium (medium_stiff), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; reinforced landing gear designed to tolerate higher touchdown loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~7.4 s with a synthetic deployment failure risk of ~9.5%. In the synthetic mission model, it cruises at about 21.9 m/s and climbs at about 4.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.19. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,7.403005017979524,0.09454883265503053,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, harpy_eagle, tiger, bat, with 10 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.9,0.9,0.1,0.9000000000000001,5
+DLIFT_b5222a249d,"bat,tiger","LIFT_BURST_POWER,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,5,22.24663246718933,69.42202767392673,7,1.1959578402021858,1.0109660543354295,5.1143714330764025,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.946870104662082,188.39092224581674,1497.1181879849998,77.87325258813135,15656.578636399441,1.9192145497338218,76.76858198935287,3070.7432795741147,electric_ducted_fan,0.9002320332475999,0.9613113956128481,56.10013088413826,steel_truss,heavy_robust,0.01,glass_composite,steel,0.8481356717271602,0.6943757330879909,1.6826673531103236,1.4194582902708006,3.0674391009020994,18.27322175761787,5.153760752620356,2,91.66866014111606,3.120563428029591,True,True,True,3.120563428029591,"Bio-inspired by bat, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 22.2 kg, and carries a payload of 69.4 kg (3.12:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.9 kg battery (~1497 Wh usable) at about 78 V. Estimated battery peak power is ~15.7 kW. It also includes ~1.9 kg of supercapacitors (~77 Wh) that can provide high peak power (up to ~3.1 kW). The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~56 A. The main frame uses steel truss (heavy_robust), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members; foldable wings that deploy after vertical takeoff for cruise efficiency; morphing lifting surface that can change camber and area for control and efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~7.7 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 18.3 m/s and climbs at about 5.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.12. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,True,7.675606518877065,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, tiger, with 7 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_58d49fe1c5,"osprey,bat,bee,dragonfly,cheetah","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,11,18.417810051036803,78.27509034667082,24,1.33729067364591,2.2211322409098035,18.06167416841673,0.051850116047600064,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.96750170662164,189.68076351103062,1700.9625704984628,30.888521789814718,14104.870674503809,1.6027233626377688,64.10893450551075,2564.35738022043,electric_multirotor_plus_pusher,0.8414061912977855,0.976454444048882,17.570271472915657,steel_truss,heavy_robust,0.01,aluminum,composite,0.7,0.6009087222918505,1.2,1.59261984214717,2.1804112071422335,5.032010508394347,5.605081773029596,4,96.69290039770763,4.249967294144422,True,True,True,4.249967294144422,"Bio-inspired by osprey, bat, bee, dragonfly, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 24 rotors, has an empty mass of 18.4 kg, and carries a payload of 78.3 kg (4.25:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.0 kg battery (~1701 Wh usable) at about 31 V. Estimated battery peak power is ~14.1 kW. It also includes ~1.6 kg of supercapacitors (~64 Wh) that can provide high peak power (up to ~2.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~18 A. The main frame uses steel truss (heavy_robust), with aluminum rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; multiple flight modes to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; a compliant spine-like frame that absorbs dynamic loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.9 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 5.0 m/s and climbs at about 5.6 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.25. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5179354357105102,1.05,0.9,0.01,True,2.911188138390923,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, bat, bee, dragonfly, cheetah, with 24 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, aluminum rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_d67e403dd5,"tiger,cheetah,dragonfly,bee","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,8,20.384735334976774,69.40622245129634,14,1.5136189804662232,1.228421321152995,3.964305903229988,0.12499150482480292,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,11.875898705535135,337.82616791488897,4011.989350236325,29.286684301559266,12431.119767715902,1.3476902865575715,53.90761146230286,2156.3044584921145,electric_brushless_outunner,0.8317229572469296,0.9562941056685428,57.61544450953899,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.6352985582345267,0.5244469314520959,1.2,1.309214911994103,3.704370477895917,24.894511717169365,5.653240145188598,4,89.79095778627311,3.404813519075077,True,True,True,3.404813519075077,"Bio-inspired by tiger, cheetah, dragonfly, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 14 rotors, has an empty mass of 20.4 kg, and carries a payload of 69.4 kg (3.40:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 11.9 kg battery (~4012 Wh usable) at about 29 V. Estimated battery peak power is ~12.4 kW. It also includes ~1.3 kg of supercapacitors (~54 Wh) that can provide high peak power (up to ~2.2 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~58 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 24.9 m/s and climbs at about 5.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.40. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, cheetah, dragonfly, bee, with 14 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.2,0.8,5
+DLIFT_828a2d75f2,"bat,albatross,tiger,golden_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",4,10,21.307314912402454,77.40559755554169,11,2.421990232988367,1.0422671923244289,11.819634583421644,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.486980460328983,252.24036203813463,1888.5186618858224,62.655160864525115,20734.37201122505,2.0216905058217027,80.8676202328681,3234.704809314724,electric_multirotor_plus_pusher,0.9161259686010085,0.9633874310657964,33.100555412066164,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.8567099713232518,0.036421736744171526,1.5284375679652813,0.6394518802082968,2.9318852869867813,9.80572472107477,4.042963972074297,6,98.71291246794414,3.6328180192468,True,True,True,3.6328180192468,"Bio-inspired by bat, albatross, tiger, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 21.3 kg, and carries a payload of 77.4 kg (3.63:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.5 kg battery (~1889 Wh usable) at about 63 V. Estimated battery peak power is ~20.7 kW. It also includes ~2.0 kg of supercapacitors (~81 Wh) that can provide high peak power (up to ~3.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~33 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; reinforced landing gear designed to tolerate higher touchdown loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.3 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 9.8 m/s and climbs at about 4.0 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.63. ",rotor_plus_pusher,multirotor,pusher_propeller,0.22944874612181285,1.05,0.9,0.01,True,2.2893121126001006,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, albatross, tiger, golden_eagle, with 11 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.5,0.5,0.4,0.52,3
+DLIFT_64282856d0,"bat,albatross,harpy_eagle,osprey,dragonfly","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,12,18.906006732237277,52.18646150446888,19,1.4588111545888118,2.169087862459283,9.981936458789065,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.661584901526908,255.65354230515447,2470.018404357351,93.2323835536296,28854.46006607226,1.9372389727843258,77.48955891137302,3099.582356454921,electric_brushless_outunner,0.841788524689172,0.9554562770984714,28.643198231024048,titanium_alloy,heavy_robust,0.005,glass_composite,steel,1.081044189234,0.0,1.7448495729866607,1.1889778752484423,2.2052215029218027,13.995071192186682,2.334147545503469,3,71.09246823670615,2.760311166899352,True,True,True,2.760311166899352,"Bio-inspired by bat, albatross, harpy_eagle, osprey, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 18.9 kg, and carries a payload of 52.2 kg (2.76:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.7 kg battery (~2470 Wh usable) at about 93 V. Estimated battery peak power is ~28.9 kW. It also includes ~1.9 kg of supercapacitors (~77 Wh) that can provide high peak power (up to ~3.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~29 A. The main frame uses titanium alloy (heavy_robust), with glass composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.6 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 14.0 m/s and climbs at about 2.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.76. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,6.567377751692854,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, albatross, harpy_eagle, osprey, dragonfly, with 19 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.2,0.72,4
+DLIFT_1fe209293c,"bat,albatross,harpy_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",3,8,22.80272620518781,77.11166074270147,10,1.4601731017897475,2.9005383126599513,10.642135893201488,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.144248117548001,248.1616129429118,1276.6049102292495,35.64780892055155,13038.963247996531,2.4707150531953825,98.8286021278153,3953.144085112612,electric_brushless_outunner,0.8725526569717124,0.9833636258132549,72.33551593001114,steel_truss,heavy_robust,0.01,aluminum,composite,0.9585271790568648,0.0,1.4185465466720841,0.9601328349881553,2.005312631135782,13.45062567057784,5.393530711105905,5,99.91438694788928,3.381686033890015,True,True,True,3.381686033890015,"Bio-inspired by bat, albatross, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 22.8 kg, and carries a payload of 77.1 kg (3.38:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.1 kg battery (~1277 Wh usable) at about 36 V. Estimated battery peak power is ~13.0 kW. It also includes ~2.5 kg of supercapacitors (~99 Wh) that can provide high peak power (up to ~4.0 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~72 A. The main frame uses steel truss (heavy_robust), with aluminum rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.4 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 13.5 m/s and climbs at about 5.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.38. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,6.362431582826874,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, albatross, harpy_eagle, with 10 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, aluminum rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_9eef80ea35,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,14.002587413033416,61.41173394989143,4,1.9968272614997706,2.026756252398351,4.212475992026451,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,11.50455918553132,343.8198269188229,3955.495547946733,42.385780155994595,32502.059015143186,2.236837189613984,89.47348758455936,3578.939503382375,electric_multirotor_plus_pusher,0.8487883107898857,0.955212841851516,148.3023073177582,carbon_composite,light_stiff,0.01,aluminum,titanium,0.7506559352155596,0.0,0.9567754259601549,1.9974231049311406,1.1501324053047501,15.388311035985963,4.427809960944469,4,75.41432136292484,4.385741873157687,True,True,True,4.385741873157687,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 14.0 kg, and carries a payload of 61.4 kg (4.39:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 11.5 kg battery (~3955 Wh usable) at about 42 V. Estimated battery peak power is ~32.5 kW. It also includes ~2.2 kg of supercapacitors (~89 Wh) that can provide high peak power (up to ~3.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~148 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 15.4 m/s and climbs at about 4.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.39. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5588621040367758,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 4 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.2,0.72,4
+DLIFT_14b2bce850,"dragonfly,osprey,bat,tiger","LIFT_BURST_POWER,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,9,19.76333816420047,64.0159712502665,9,1.9729505658110127,1.6851786409006533,3.25597206228753,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.549755997635359,244.56531444401782,2090.973763981319,95.08963534444946,17366.07195360235,0.07894256114152376,3.1577024456609504,126.30809782643801,electric_multirotor_plus_pusher,0.8108411013532123,0.953235645121047,10.220945575782162,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.8332863205237694,0.13136510011580607,1.2,3.6233537549746586,2.570089346186293,7.5887406578878664,5.870064455883301,4,83.77930941446698,3.2391274550078664,True,True,True,3.2391274550078664,"Bio-inspired by dragonfly, osprey, bat, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 19.8 kg, and carries a payload of 64.0 kg (3.24:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.5 kg battery (~2091 Wh usable) at about 95 V. Estimated battery peak power is ~17.4 kW. It also includes ~0.1 kg of supercapacitors (~3 Wh) that can provide high peak power (up to ~0.1 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~10 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads. It uses foldable wings that deploy after takeoff. The wing deployment time is ~5.9 s with a synthetic deployment failure risk of ~11.2%. In the synthetic mission model, it cruises at about 7.6 m/s and climbs at about 5.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.24. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5998643028417444,1.05,0.9,0.01,True,5.851816011868021,0.11194827353616746,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, osprey, bat, tiger, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_9c2aa4914d,"bee,bat,dragonfly,tiger,cheetah","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,10,14.93225850102178,75.20797951982158,8,2.474318267811226,1.6661348214640137,15.298490153201454,0.21299000146886962,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.352207421261374,222.83214944831516,969.8117345245809,43.27930510317173,9192.043034722827,0.25272647109697455,10.109058843878982,404.3623537551593,electric_multirotor_plus_pusher,0.9091175524800603,0.9618772941624255,20.67627660015485,carbon_composite,light_stiff,0.01,aluminum,steel,0.7,0.36998465879092224,1.5922752732560823,0.5699200033430095,1.5883738851491451,6.560763135456787,5.543990999441754,5,90.14023802084336,5.03661114055019,True,True,True,5.03661114055019,"Bio-inspired by bee, bat, dragonfly, tiger, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 14.9 kg, and carries a payload of 75.2 kg (5.04:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.4 kg battery (~970 Wh usable) at about 43 V. Estimated battery peak power is ~9.2 kW. It also includes ~0.3 kg of supercapacitors (~10 Wh) that can provide high peak power (up to ~0.4 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~21 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics for better hover and low-speed lift; multiple flight modes to optimize heavy-load and unloaded segments; a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. It uses foldable wings that deploy after takeoff. The wing deployment time is ~6.6 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 6.6 m/s and climbs at about 5.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.04. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4798793794240107,1.05,0.9,0.01,True,6.631273959015552,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, bat, dragonfly, tiger, cheetah, with 8 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_d21a7b6653,"bat,tiger","LIFT_BURST_POWER,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,5,14.982960951719281,66.30779540997813,11,1.349732606034011,2.7464821282311638,8.97715965073108,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.047901226799402,231.15118676785687,704.5259857258886,60.18994410595072,2936.966553423279,0.9753209731886753,39.01283892754701,1560.5135571018805,electric_multirotor_plus_pusher,0.9189637301893897,0.9406818036158104,5.60623923968096,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.95074295048691,0.05103462546039504,1.9237042927075287,2.9881744560721533,1.0251857900418788,12.280395292811638,5.313177535195178,5,81.2907563616974,4.425546834410548,True,True,True,4.425546834410548,"Bio-inspired by bat, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 15.0 kg, and carries a payload of 66.3 kg (4.43:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.0 kg battery (~705 Wh usable) at about 60 V. Estimated battery peak power is ~2.9 kW. It also includes ~1.0 kg of supercapacitors (~39 Wh) that can provide high peak power (up to ~1.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~6 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members; foldable wings that deploy after vertical takeoff for cruise efficiency; morphing lifting surface that can change camber and area for control and efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~4.2 s with a synthetic deployment failure risk of ~11.4%. In the synthetic mission model, it cruises at about 12.3 m/s and climbs at about 5.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.43. ",rotor_plus_pusher,multirotor,pusher_propeller,0.3449350713031284,1.05,0.9,0.01,True,4.212096163304878,0.11406022423757685,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, tiger, with 11 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_80d4fb0980,"tiger,albatross,dragonfly","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,8,18.80752450910986,50.771012888880065,10,1.7854674258335348,2.270250932236621,17.798938495354793,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus lithium-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,11.158964324291697,625.2893983306982,6977.582088330081,54.30020476467449,20625.254011580226,1.324976764581419,52.99907058325676,2119.9628233302706,electric_brushless_outunner,0.8554542951452498,0.9568737938254174,60.36070090551491,carbon_composite,light_stiff,0.01,aluminum,titanium,0.5874372069682171,0.31266320344552695,1.3949074028639055,1.5622087076574724,1.9222277083250079,19.864551568454846,2.303191052579288,3,69.57853739798992,2.6995053423584774,True,True,True,2.6995053423584774,"Bio-inspired by tiger, albatross, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 18.8 kg, and carries a payload of 50.8 kg (2.70:1 payload-to-aircraft mass ratio). The energy system is fuel-cell-li-ion-hybrid with a 11.2 kg battery (~6978 Wh usable) at about 54 V. Estimated battery peak power is ~20.6 kW. It also includes ~1.3 kg of supercapacitors (~53 Wh) that can provide high peak power (up to ~2.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~60 A. The main frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads. In the synthetic mission model, it cruises at about 19.9 m/s and climbs at about 2.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.70. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, albatross, dragonfly, with 10 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.0,0.8400000000000001,5
+DLIFT_a4b8ee5665,bee,"LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST",1,2,15.413940515515996,54.427628771751245,9,1.3275354260456624,1.0,0.0,0.05480457827610291,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.758953775299756,218.5027633477683,1258.3473138950594,58.023095269394744,9824.91624749236,0.0,0.0,0.0,electric_brushless_outunner,0.7850679383853408,0.9534756050465029,24.857021698234213,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.3882714015514136,0.0,0.8310112257460806,1.2203470978236404,0.5365164534584714,10.541120236210045,2.5295174130431373,2,69.84156928726725,3.5310651884872173,True,True,True,3.5310651884872173,"Bio-inspired by bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 15.4 kg, and carries a payload of 54.4 kg (3.53:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 5.8 kg battery (~1258 Wh usable) at about 58 V. Estimated battery peak power is ~9.8 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~25 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include unsteady aerodynamics for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy. In the synthetic mission model, it cruises at about 10.5 m/s and climbs at about 2.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.53. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, with 9 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_b7fb8c9316,"tiger,osprey,albatross,harpy_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",4,11,19.695902151694188,65.84299034460837,10,1.9602156469941563,1.810229117599057,3.31423152521271,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,3.3819253099264577,318.9130232914443,1078.5400251345013,50.24147665308408,8027.7534004840045,1.3356605568880666,53.42642227552267,2137.0568910209067,electric_brushless_outunner,0.8450266594454265,0.9542616266063707,26.99736792236688,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.8473868603633277,0.44417146496948406,1.2,1.4677749803798585,2.0084678044645985,13.690080648555188,3.291325780552242,4,85.53889249630255,3.34297915563846,True,True,True,3.34297915563846,"Bio-inspired by tiger, osprey, albatross, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 19.7 kg, and carries a payload of 65.8 kg (3.34:1 payload-to-aircraft mass ratio). The energy system is solid-state with a 3.4 kg battery (~1079 Wh usable) at about 50 V. Estimated battery peak power is ~8.0 kW. It also includes ~1.3 kg of supercapacitors (~53 Wh) that can provide high peak power (up to ~2.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~27 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight. In the synthetic mission model, it cruises at about 13.7 m/s and climbs at about 3.3 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.34. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, albatross, harpy_eagle, with 10 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.2,0.72,4
+DLIFT_58b0bd4af6,"golden_eagle,tiger,osprey","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,8,14.022278304848111,56.06727258467499,10,1.8287226517075428,1.8408006367032053,14.40261932549848,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.704321476268588,255.71335103484668,1714.384511111531,27.844626313545845,9658.067522622589,1.9483576756831427,77.9343070273257,3117.372281093028,electric_ducted_fan,0.7829574711562475,0.9833128186215785,70.90000135732679,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.32139476994382143,0.3774349226774951,1.2,1.3153302440548555,2.980547469933217,23.605017472092378,5.241519300079208,4,70.0895508895231,3.9984424332307036,True,True,True,3.9984424332307036,"Bio-inspired by golden_eagle, tiger, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 14.0 kg, and carries a payload of 56.1 kg (4.00:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.7 kg battery (~1714 Wh usable) at about 28 V. Estimated battery peak power is ~9.7 kW. It also includes ~1.9 kg of supercapacitors (~78 Wh) that can provide high peak power (up to ~3.1 kW). The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~71 A. The main frame uses magnesium alloy (very_light_fragile), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 23.6 m/s and climbs at about 5.2 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.00. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, tiger, osprey, with 10 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.6,0.6,0.2,0.64,4
+DLIFT_afb77b7cf7,"osprey,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",2,6,14.73345899788108,74.36086330788677,4,1.328335973569383,1.7750310348776541,19.142308941113818,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.180441885117814,184.1722032936653,585.7489894296061,85.43519125529423,4025.679691466248,0.35140167905053155,14.056067162021261,562.2426864808505,electric_multirotor_plus_pusher,0.8624834732651556,0.9520485762680858,11.467527118949187,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.5298579659687794,0.0,1.2,3.897240034190091,2.2102341237987737,9.029056898085638,5.053738303903119,6,89.09432230576786,5.047074371237679,True,True,True,5.047074371237679,"Bio-inspired by osprey, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 14.7 kg, and carries a payload of 74.4 kg (5.05:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 3.2 kg battery (~586 Wh usable) at about 85 V. Estimated battery peak power is ~4.0 kW. It also includes ~0.4 kg of supercapacitors (~14 Wh) that can provide high peak power (up to ~0.6 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~11 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 9.0 m/s and climbs at about 5.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.05. ",rotor_plus_pusher,multirotor,pusher_propeller,0.2923223233052413,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, harpy_eagle, with 4 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,1.0,0.0,3
+DLIFT_a6c3cc6659,"golden_eagle,cheetah,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",3,8,15.412878120981429,59.912184776649134,22,1.7913351685938435,1.895969232886914,17.51767166981076,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.48008302893112,217.9583436615681,1630.3465074368323,24.038206614805276,17119.61059692014,2.174036125158197,86.96144500632789,3478.4578002531157,electric_brushless_outunner,0.8100125341948698,0.9424256846948585,59.90118028704024,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.7,0.24552109065142813,1.8576806602511937,2.2578829090254113,0.962096431559375,12.942498967145372,4.036359625011025,5,75.32506289763056,3.88715101140592,True,True,True,3.88715101140592,"Bio-inspired by golden_eagle, cheetah, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 15.4 kg, and carries a payload of 59.9 kg (3.89:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.5 kg battery (~1630 Wh usable) at about 24 V. Estimated battery peak power is ~17.1 kW. It also includes ~2.2 kg of supercapacitors (~87 Wh) that can provide high peak power (up to ~3.5 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~60 A. The main frame uses titanium alloy (heavy_robust), with carbon composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy. In the synthetic mission model, it cruises at about 12.9 m/s and climbs at about 4.0 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.89. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, cheetah, dragonfly, with 22 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.9,0.9,0.1,0.9000000000000001,5
+DLIFT_b65bb488f2,"dragonfly,harpy_eagle,albatross,bat,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,13,20.836838841992908,61.68710606888946,22,1.8663839345902888,1.240135694526297,14.649198210542236,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.738033508842697,248.90065514879424,2174.902265063065,56.202994372619536,22473.329412953608,1.2681934283940732,50.72773713576293,2029.1094854305172,electric_brushless_outunner,0.8929953245739102,0.9448136398635545,27.636688087989313,aluminum_lithium,medium_stiff,0.02,glass_composite,titanium,0.39118869564601394,0.6977809235457934,1.722184728727784,2.1316239687313936,1.205217505091232,10.7968140040526,2.8978931844790083,4,82.52394491088236,2.9604829473734844,True,True,True,2.9604829473734844,"Bio-inspired by dragonfly, harpy_eagle, albatross, bat, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 20.8 kg, and carries a payload of 61.7 kg (2.96:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 8.7 kg battery (~2175 Wh usable) at about 56 V. Estimated battery peak power is ~22.5 kW. It also includes ~1.3 kg of supercapacitors (~51 Wh) that can provide high peak power (up to ~2.0 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~28 A. The main frame uses aluminum lithium (medium_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; multiple flight modes to optimize heavy-load and unloaded segments; a central payload cradle aligned with the center of gravity. It uses foldable wings that deploy after takeoff. The wing deployment time is ~4.2 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 10.8 m/s and climbs at about 2.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.96. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,4.219213393053589,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, harpy_eagle, albatross, bat, cheetah, with 22 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_72bbcbb2e6,"dragonfly,tiger","LIFT_BURST_POWER,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,5,12.45499008821928,69.5813770317348,8,1.3568819178943037,1.1553308052558215,19.52958663086296,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus lithium-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,10.993765607692865,512.6351367975674,5635.790536220024,28.242616491007343,14850.88215573827,0.6404480134886696,25.617920539546787,1024.7168215818715,electric_brushless_outunner,0.7821612047914213,0.9568656789464732,94.17736810063586,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.9061751848691612,0.6949909741163556,1.4453171842419272,4.008377720409462,2.386192655903134,11.300015139046678,2.780413736252346,3,82.03636711995408,5.5866264476235346,True,True,True,5.5866264476235346,"Bio-inspired by dragonfly, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 12.5 kg, and carries a payload of 69.6 kg (5.59:1 payload-to-aircraft mass ratio). The energy system is fuel-cell-li-ion-hybrid with a 11.0 kg battery (~5636 Wh usable) at about 28 V. Estimated battery peak power is ~14.9 kW. It also includes ~0.6 kg of supercapacitors (~26 Wh) that can provide high peak power (up to ~1.0 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~94 A. The main frame uses steel truss (heavy_robust), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads; a tendon or cable-based structural system to save mass in tension members. In the synthetic mission model, it cruises at about 11.3 m/s and climbs at about 2.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.59. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, tiger, with 8 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.8,0.8,0.1,0.8200000000000001,5
+DLIFT_2f7ca6b01a,"albatross,harpy_eagle,tiger","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,8,13.599742972168311,77.306509042034,8,1.5416329458112628,1.0772882175702514,9.51405068758639,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,9.113925450036556,439.34949897361423,4004.1985801564324,59.88057412877702,13409.58455011465,2.795423161740076,111.81692646960303,4472.677058784121,electric_ducted_fan,0.8685477389897366,0.9538418837775603,62.241185480886415,carbon_composite,light_stiff,0.01,glass_composite,titanium,1.0723280899017162,0.10945818039428094,0.9011797135048464,1.1274953391634583,1.320797584095484,22.892238382964955,5.738534780327135,6,90.90625201420231,5.684409565698463,True,True,True,5.684409565698463,"Bio-inspired by albatross, harpy_eagle, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 13.6 kg, and carries a payload of 77.3 kg (5.68:1 payload-to-aircraft mass ratio). The energy system is li-s with a 9.1 kg battery (~4004 Wh usable) at about 60 V. Estimated battery peak power is ~13.4 kW. It also includes ~2.8 kg of supercapacitors (~112 Wh) that can provide high peak power (up to ~4.5 kW). The primary propulsion architecture is ducted fans hybrid, using electric ducted fan motors with a nominal electronic speed controller rating of ~62 A. The main frame uses carbon composite (light_stiff), with glass composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central payload cradle aligned with the center of gravity; reinforced landing gear designed to tolerate higher touchdown loads. In the synthetic mission model, it cruises at about 22.9 m/s and climbs at about 5.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.68. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, harpy_eagle, tiger, with 8 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.7,0.7,0.3,0.7,4
+DLIFT_3c1d7801c3,albatross,"LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_HIGH_ASPECT",1,3,14.293809404283877,67.4251855032747,5,1.1096370165309246,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.69296778475602,227.13199169481774,1520.187103300887,36.31653097870023,6565.4352875125,0.0,0.0,0.0,electric_brushless_outunner,0.8698596811298327,0.9590903563129594,46.3800507695044,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.9177020734437566,0.0,0.8943398272782216,1.0490867639860397,0.7046510992686879,6.870514457281871,5.116225287542237,4,81.71899490755858,4.717090007025508,True,True,True,4.717090007025508,"Bio-inspired by albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 14.3 kg, and carries a payload of 67.4 kg (4.72:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.7 kg battery (~1520 Wh usable) at about 36 V. Estimated battery peak power is ~6.6 kW. The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~46 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and steel landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic mission model, it cruises at about 6.9 m/s and climbs at about 5.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.72. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, with 5 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers.",0.0,0.0,0.9,0.019999999999999997,3