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Matches in DBpedia 2014 for { ?s <http://dbpedia.org/property/moreGeneral> ?o. }

• Grumman_F6F_Hellcat moreGeneral "*Fuel capacity: 250 gal internal; up to 3 × 150 gal external drop tanks *Zero-lift drag coefficient: 0.0211 *Drag area: 7.05 ft² *Aspect ratio: 5.5".
• Grumman_HU-16_Albatross moreGeneral "Fuel Capacity: 675 US Gallons internally, plus 400 US Gal in wingtip floats plus two 300 US Gallon drop tanks".
• Gulfstream_G550 moreGeneral "Maximum Ramp Weight: 85,500 lb *Maximum landing weight: 75,300 lb *Maximum fuel weight: 35,200 lb *Cabin dimensions: volume: 1,669 ft³ , height: 6 ft 2 in , width: 7 ft 4 in *Baggage compartment volume: 226 ft³".
• Gulfstream_G550 moreGeneral "Maximum Ramp Weight: 91,400 lb *Maximum landing weight: 75,300 lb *Maximum fuel weight: 41,300 lb *Cabin dimensions: volume: 1,669 ft³ , height: 6 ft 2 in , width: 7 ft 4 in *Baggage compartment volume: 226 ft³".
• Gulfstream_G650 moreGeneral "Maximum landing weight: 83,500 lb *Wing sweep: 36 degrees".
• Gulfstream_V moreGeneral "Maximum landing weight: 75,300 lb * Maximum fuel weight: 41,300 lb * Cabin dimensions: length - 50 ft 1 in , height - 6 ft 2 in , width - 7 ft 4 in * Volumes: cabin - 1,669 ft³ , baggage compartment - 226 ft³".
• HAL_Tejas moreGeneral "Internal fuel capacity: 2,458 kg * External fuel capacity: 2 x 1,200 litre drop tank at inboard, 1 x 725-litre drop tank under fuselage".
• Handley_Page_Type_W moreGeneral ", and 2 x 240 hp Siddeley Puma engines".
• Hawker_Duiker moreGeneral "Designed Maximum Weight: 4,940 lb".
• Hawker_Tornado moreGeneral "*Fuel capacity: 140 gallons".
• Heavy_Transport_Helicopter moreGeneral "192.0".
• Heinkel_He_162 moreGeneral "Fuel capacity of 695 litres".
• Heinkel_He_277 moreGeneral "maximum of 16,950 litre/4,478 US gallon fuel/consumables capacity for Amerika Bomber mission profile".
• Henschel_Hs_130 moreGeneral "one Daimler-Benz DB 605T, driving HZ-Anlange supercharger in fuselage".
• Hill_Tetra-15 moreGeneral "Performance".
• Hiller_YROE moreGeneral "*Fuel: 9.1 L".
• Hordern-Richmond_Autoplane moreGeneral "Folded width: 17 ft 10 in".
• Horten_H.III moreGeneral "*Chord at root: *Sweep at root: 24.3 degrees *Aerofoil thickness: 20%".
• Horten_H.IV moreGeneral "*Aerofoil thickness: 16% *Sweepback at LE: 20 degrees".
• Horten_H.XVIII moreGeneral "*Leading edge sweepback: 24.3 * Aerofoil thickness: 16%".
• I.Ae._34_Clen_Antú moreGeneral "*Leading edge sweepback: 21.8 degrees *Aerofoiul thickness: 18%".
• I.Ae._41_Urubú moreGeneral "*Leading edge sweepback: 26.6 * Aerofoil thickness: 18%".
• IAR_316 moreGeneral "156.0".
• Ilyushin_Il-114 moreGeneral "*Useful load: :::Il-114T:".
• Ilyushin_Il-18 moreGeneral "* Fuselage diameter: * Max. landing weight: * Max. zero-fuel weight: * Max. taxi weight :".
• Ilyushin_Il-62 moreGeneral "Fuel: 105,300 L".
• Ilyushin_Il-78 moreGeneral "*Special equipment: 3 x UPAZ-1M 'Sakhalin', , refuelling pods; Two on pylons under the outer wings, and the third on the port side of the rear fuselage. *Fuel transfer rate: up to 1361 kg/min".
• Intermediate_eXperimental_Vehicle moreGeneral "Power: Batteries".
• Ion_Aircraft_Ion moreGeneral "*Useful load: 552 lb".
• Junkers_W_33 moreGeneral "cargo hold volume 15.7 m3, : could carry 830 kg cargo".
• Kaman_SH-2G_Super_Seasprite moreGeneral "Rotor systems: 4 blades on main rotor and tail rotor".
• Kaman_SH-2_Seasprite moreGeneral "Rotor systems: 4 blades on main rotor and 3 on tail rotor".
• Kaman_SH-2_Seasprite moreGeneral "Rotor systems: 4 blades on main rotor and tail rotor".
• Kestrel_JP10 moreGeneral "*Pressurization: *Maximum cabin altitude: at FL 310".
• Lancair_Propjet moreGeneral "Aspect Ratio: 9:1 * Propeller: 3 blade, constant speed * Fuel Capacity: 125 gallons ; 145 gallons * Baggage Capacity: 150 lb * Cabin Width: 46 in ; 43 in * Height: 48 in".
• Laubenthal_Lore moreGeneral "* Wing loading: 16 kg/m²".
• Laubenthal_Württemberg moreGeneral "* Wing loading: 15 kg/m²".
• Learjet_35 moreGeneral "*Fuel capability: 931 US gallons".
• Learjet_35 moreGeneral "*Unit cost: $3.1 million".
• Learjet_40 moreGeneral "Cabin Height: 4.9 ft * Cabin Width: 5.1 ft * Cabin Length: 19.75 ft * Cabin Volume: 368 ft³ * Door Height: 4.8 ft * Door Width: 2.5 ft * Baggage Volume Internal: 15 ft³ * Baggage Volume External: 50 ft³ * Maximum Landing Weight: 19,200 lb * Usable Fuel: 5,325 lb * Payload with Full Fuel: 993 lb * Maximum Payload: 2,305 lb".
• Letov_LK-2_Sluka moreGeneral "50".
• Lioré_et_Olivier_LeO_45 moreGeneral "Fuel capacity: 3,235 l".
• Lockheed_A-12 moreGeneral "Payload: 2,500 lb of reconnaissance sensors".
• Lockheed_AH-56_Cheyenne moreGeneral "Rotor systems: 4 blades on main rotor, 4 blades on tail rotor, 3 blades on pusher propeller".
• Lockheed_F-104_Starfighter moreGeneral "Zero-lift drag coefficient: 0.0172 * Drag area: 3.37 sq ft * Aspect ratio: 2.45".
• Lockheed_Martin_F-22_Raptor moreGeneral "Fuel capacity: 18,000 lb internally, or 26,000 lb with two external fuel tanks. About 3,050 gal or 20,333 lb JP-8 internally.".
• Lockheed_Martin_F-35_Lightning_II moreGeneral "Internal fuel capacity: 18,480 lb".
• Lockheed_P-38_Lightning moreGeneral "Zero-lift drag coefficient: 0.0268 * Drag area: 8.78 ft² * Aspect ratio: 8.26".
• Lockheed_P-80_Shooting_Star moreGeneral "Zero-lift drag coefficient: 0.0134 * Drag area: 3.2 ft²".
• Lockheed_S-3_Viking moreGeneral "Internal fuel capacity: 1,933 US gal of JP-5 fuel *External fuel capacity: 2x 300 US gal tanks".
• Lockheed_SR-71_Blackbird moreGeneral "Wheel track: *Wheelbase: *Aspect ratio: 1.7".
• Lockheed_TriStar_(RAF) moreGeneral "Maximum Fuel Load: 136,080 kg".
• MD_Helicopters_MH-6_Little_Bird moreGeneral "Fuselage Length: 24.6 ft *Fuselage Width: 4.6 ft *Rotor systems: 6 blades on main rotor, 4 blades on tail rotor *Useful fuel capacity: 62 US gal or 403 lb".
• Martin_B-57_Canberra moreGeneral "*Zero-lift drag coefficient: 0.0119 *Drag area: 11.45 ft² *Aspect ratio: 4.27".
• Martin_Jetpack moreGeneral "Fuel capacity: 5 US gallons".
• Mason_Greater_Meteor moreGeneral "original".
• McDonnell_Douglas_A-12_Avenger_II moreGeneral "Maximum fuel capacity:".
• McDonnell_Douglas_F-15_Eagle moreGeneral "Fuel capacity: 13,455 lb internal".
• MTD moreGeneral "*Fuel capacity: 11,520 lb *Horizontal tail span: 28.2 ft *Canard span: 25.6 ft".
• McDonnell_Douglas_F-4_Phantom_II moreGeneral "Zero-lift drag coefficient: 0.0224 *Drag area: 11.87 ft² *Aspect ratio: 2.77 *Fuel capacity: 1,994 U.S. gal internal, 3,335 U.S. gal with three external tanks . *Maximum landing weight: 36,831 lb".
• A-18_Hornet moreGeneral "Fuel capacity: internally".
• McDonnell_Douglas_KC-10_Extender moreGeneral "Maximum fuel capacity: 356,000 lb".
• McDonnell_F-101_Voodoo moreGeneral "Internal fuel capacity: 2,053 gal or 2,953 gal with two external tanks".
• McDonnell_FH_Phantom moreGeneral "Fuel capacity: 375 gal internal, 670 gal with external drop tank".
• Merville_D.63 moreGeneral "*Maximimum wing loading: 61 kg/m2 *Maximum power loading: 14.8 lb/hp".
• Merville_SM.31 moreGeneral "*Maximum wing loading: 25.5 kg/m2".
• Messerschmitt_Me_262 moreGeneral "Aspect ratio: 7.32".
• Messerschmitt_P.1101 moreGeneral "* Fuel capacity : about 370 gallons".
• Mikoyan-Gurevich_MiG-105 moreGeneral "500".
• Mil_Mi-10 moreGeneral "Ground clearance under fuselage:".
• Mil_Mi-6 moreGeneral "Fuel load: 6,315 kg".
• Mil_Mi-8 moreGeneral "Fuel max total capacity: 3,700 l".
• Mil_V-12 moreGeneral "*Freight compartment:".
• Miles_M.39B_Libellula moreGeneral "*Sweepback on leading edge rear wing 21° 0′ 48″".
• Mitsubishi_A6M_Zero moreGeneral "Aspect ratio: 6.4".
• Mitsubishi_F-15J moreGeneral "Fuel capacity: 13,455 lb internal".
• Musger_Mg_9 moreGeneral "*Wing loading:19.8 kg/m2".
• Naval_Aircraft_Factory_TF moreGeneral "Fuel capacity:".
• North_American_F-100_Super_Sabre moreGeneral "*Zero-lift drag coefficient: 0.0130 *Drag area: 5.0 ft² *Aspect ratio: 3.76".
• North_American_F-86_Sabre moreGeneral "Fuel provisions Internal fuel load: ), Drop tanks: 2x JP-4 fuel".
• North_American_FJ-1_Fury moreGeneral "Fuel provisions Internal fuel load: 465 gal , Wing Tip Tanks: 2 × 170 gal".
• North_American_P-51_Mustang moreGeneral "Zero-lift drag coefficient: 0.0163 *Drag area: 3.80 sqft *Aspect ratio: 5.83".
• North_American_Rockwell_OV-10_Bronco moreGeneral "Tailplane Span 14 ft, 7 in".
• North_American_XB-70_Valkyrie moreGeneral "Internal fuel capacity: 300,000 lb or 46,745 US gallons".
• Northrop_F-5 moreGeneral "Zero-lift drag coefficient: 0.0200 * Drag area: 3.4 ft² * Aspect ratio: 3.86 * Internal fuel: 677 U.S. gal * External fuel: 275 U.S. gal per tank in up to 3 tanks".
• Northrop_Grumman_B-2_Spirit moreGeneral "Fuel Capacity: 167,000 pounds".
• Northrop_P-61_Black_Widow moreGeneral "Fuel capacity: **Internal: 640 gal of AN-F-48 100/130-octane rating gasoline **External: Up to four 165 gal or 310 gal tanks under the wings".
• Oberlerchner_Mg_19 moreGeneral "*Maximum wing loading: 22.9 kg/m2".
• OpenSky_M-02 moreGeneral "Mean aerodynamic chord: 1287 mm * Aspect ratio: 3.74 * L/D ratio: 18 * Fuel capacity: 10 L".
• Operational_Requirement_F.155 moreGeneral "Fuel: kerosene, HTP".
• PAC_MFI-17_Mushshak moreGeneral "Landing gear: fixed tricycle".
• PIK-26 moreGeneral "Fuel Capacity 27".
• PWS-22 moreGeneral "*Useful load:'".
• PZL-105_Flaming moreGeneral "Fuel: 270 L".
• Panha_2091 moreGeneral "Rotor systems: 2 blades on main rotor, 2 blades on tail rotor".
• Parajet_Skycar moreGeneral "Wing: Custom-made Paramania Reflex Wing".
• Parnall_Panther moreGeneral "Folded length: 14 ft 6 in".
• Pilatus_PC-12 moreGeneral "160.2".
• Piper_PA-12 moreGeneral "* Propellor Diameter: 76 in * Wing Chord: 63 in * Baggage Capacity: 41 lb".
• Piper_PA-44_Seminole moreGeneral "Fuel: two main nacelle tanks, each of 55 U.S. gallon capacity , two U.S. gallons unusable.".

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