Matches in DBpedia 2016-04 for { ?s <http://dbpedia.org/property/moreGeneral> ?o }
- Emelyanov_KIM-3_Stakanovets moreGeneral "*Wing loading: 19.7 kg/m²".
- English_Electric_Ayr moreGeneral "All weights estimated".
- Epic_E1000 moreGeneral "*Cabin altitude: 8,000ft at 31,000ft *Cabin height: 4.9ft *Cabin width: 4.6ft *Cabin length: 15ft".
- Eta_(glider) moreGeneral "*Maximum wing loading: 44.8 kg/m2".
- Eurocopter_Tiger moreGeneral "Internal fuel capacity: 1,080 kg".
- Eurofighter_Typhoon moreGeneral "Fuel capacity: internal".
- Extra_EA-300 moreGeneral "Fuel capacity: 199.5 l".
- F.V.D._Doris moreGeneral "*Wing loading:".
- F.V.D._Stehaufchen moreGeneral "*Wing loading:".
- FFA_AS-202_Bravo moreGeneral "Landing gear: fixed tricycle".
- FFA_AS-202_Bravo moreGeneral "Max landing weight : AS 202-18A4 1,050 kg".
- FK-Lightplanes_SW51_Mustang moreGeneral "useable".
- Fairchild_Republic_A-10_Thunderbolt_II moreGeneral "Internal fuel capacity: 11,000 lb".
- Fairchild_T-46 moreGeneral "Internal fuel capacity: 200 US Gal".
- Fairey_Long-range_Monoplane moreGeneral "Mean chord: 11 ft".
- Fajr_F.3 moreGeneral "75.0".
- Fokker_Dr.I moreGeneral "Zero-lift drag coefficient: 0.0323 *Drag area: 0.62 m2 *Aspect ratio: 4.04".
- Fouga_CM.10 moreGeneral "*Cargo hold capacity:".
- Freedom_Aviation_Phoenix moreGeneral "* Cabin width: * Cabin height: * Cabin length:".
- Gee_Bee_Model_R moreGeneral "Aspect ratio: 6.1 , *Incidence: 2.5 Degrees".
- Grumman_EF-111A_Raven moreGeneral "Zero-lift drag coefficient: 0.0186 *Drag area: 9.36 ft2 *Aspect ratio: 7.56 unswept; 1.95 fully swept".
- General_Dynamics_F-111C moreGeneral "Zero-lift drag coefficient: 0.0186 * Drag area: 9.36 ft² * Aspect ratio: spread: 7.56, swept: 1.95".
- General_Dynamics_F-111_Aardvark moreGeneral "Zero-lift drag coefficient: 0.0186 * Drag area: 9.36 ft² * Aspect ratio: spread: 7.56, swept: 1.95".
- Glaser-Dirks_DG-400 moreGeneral "*Water ballast:".
- Glaser-Dirks_DG-600 moreGeneral "*Water ballast: in two wing tanks + in fin tank for trimming.".
- 39 moreGeneral "Fuel capacity: 81 gallons".
- Grob_G_115 moreGeneral "Max Fuel Capacity: 143 L".
- Grumman_A-6_Intruder moreGeneral "Zero-lift drag coefficient: 0.0144".
- Grumman_F-14_Tomcat moreGeneral "Maximum fuel capacity: 16,200 lb internal; 20,000 lb with 2x 267 gallon external tanks".
- 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_G500_(2015) moreGeneral "Maximum landing weight: 64,350 lb".
- 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".
- Hannover_Greif moreGeneral "*Wing loading:".
- 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 "1800.0".
- Heinkel_He_277 moreGeneral "maximum of 16,950 litre/4,478 US gallon fuel/fluid-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%".
- Hydra_Technologies_Ehécatl moreGeneral "Powerplant".
- I.Ae._34_Clen_Antú moreGeneral "*Leading edge sweepback: 21.8 degrees *Aerofoil thickness: 18%".
- I.Ae._41_Urubú moreGeneral "*Leading edge sweepback: 26.6 * Aerofoil thickness: 18%".
- IAR_316 moreGeneral "156.0".
- 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: 900 to 2,200 liters/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".
- Kinner_Sportster moreGeneral "*Load:".
- Kinner_Sportwing moreGeneral "*Load:".
- 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".
- Latham_HB.5 moreGeneral "*Useful load:".
- Laubenthal_Württemberg moreGeneral "* Wing loading: 15 kg/m²".
- Learjet_35 moreGeneral "*Fuel capacity:".
- 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: internally, or with two external fuel tanks".
- Lockheed_Martin_F-35_Lightning_II moreGeneral "Internal fuel capacity: 18,498 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: 2 × 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".
- Loessl_Sb.1_Münchener_Eindekker moreGeneral "*Wing loading: 8.45 kg/m2".
- Lore_(glider) moreGeneral "* Wing loading: 16 kg/m²".
- 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".
- MX_Aircraft_MXS moreGeneral "Fuel capacity long range : 295.26 l".
- MX_Aircraft_MXS moreGeneral "Fuel capacity: 219.55 l".
- Marenco_Swisshelicopter_SKYe_SH09 moreGeneral "* Rotor systems: 5 blades on bearingless main rotor, shrouded 120cm tail rotor".
- 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: 45 Litres".
- 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".