Matches in DBpedia 2016-04 for { ?s <http://dbpedia.org/property/moreGeneral> ?o }
- 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 :".
- Mikoyan-Gurevich_MiG-105 moreGeneral "500".
- Mikoyan_MiG-29 moreGeneral "Fuel capacity: 3,500 kg. internal".
- Mil_Mi-10 moreGeneral "Ground clearance under fuselage:".
- Mil_Mi-26 moreGeneral "Main rotor RPM: 132".
- 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_NA-64_Yale moreGeneral "*Oil capacity 9.5 US gallon/36L".
- North_American_P-51_Mustang moreGeneral "*Maximum fuel capacity: *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: 3.82 * 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".
- Pelzner_Hang_Glider moreGeneral "*Wing loading: 6.4 kg/m2 )".
- 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.".
- Piper_PA-44_Seminole moreGeneral "Maximum Ramp Weight: 3 816 lb".
- Piper_PA-47_PiperJet moreGeneral "*Full fuel payload: intended to be 800 lbs +/-5%".
- Pipistrel_Sinus moreGeneral "* Fuel capacity: 2×30 L * Baggage capacity:".
- Polikarpov_TIS moreGeneral "*Fuel capacity:".
- Reaction_Engines_A2 moreGeneral "Fuel capacity: 198 tonnes liquid hydrogen".
- Republic_F-105_Thunderchief moreGeneral "Zero-lift drag coefficient: 0.0173 *Drag area: 6.65 ft² *Aspect ratio: 3.16".
- Robinson_R22 moreGeneral "Main tank total capacity: 19.8 US gallons * Main tank usable capacity: 19.2 US gallons * Optional aux tank total capacity: 10.9 US gallons * Optional aux tank usable capacity: 10.5 US gallons".
- Robinson_R44 moreGeneral "Fuel: 100 low lead fuel or 100/130. *Main tank capacity: 31.6 US gallons *Main tank usable fuel: 30.6 US gallons *Auxiliary tank capacity: 18.5 US gallons *Auxiliary tank usable fuel: 18.3 US gallons".
- Rockwell_B-1_Lancer moreGeneral "Fuel capacity, optional: 10,000 U.S. gal fuel tank each in 1–3 internal weapons bays".
- Rolladen-Schneider_LS1 moreGeneral "*Water ballast:".
- Rolladen-Schneider_LS4 moreGeneral "*Water ballast: ::::LS4-a:".
- Rolladen-Schneider_LS6 moreGeneral "*Water ballast: ::::LS6-a:".
- SZD-42_Jantar_2 moreGeneral "*Water ballast:".
- 3 moreGeneral "*Water ballast:".
- Saab_JAS_39_Gripen moreGeneral "144.0".
- Scaled_Composites_Model_367_BiPod moreGeneral "1.2".
- Schempp-Hirth_Discus moreGeneral "*Water ballast:".
- Schempp-Hirth_Janus moreGeneral "*Water ballast:".
- Schempp-Hirth_Nimbus-3 moreGeneral "*Water ballast:".
- Schempp-Hirth_Ventus moreGeneral "*Water ballast:".
- Schleicher_ASG_32 moreGeneral "*Pilot Capacity: One or two people, up to 120 kg each".
- Schleicher_ASH_25 moreGeneral "*Water ballast:".
- Schleicher_ASW_20 moreGeneral "*Water ballast: ::::ASW20C ::::ASW20BL".
- Schleicher_ASW_22 moreGeneral "*Water ballast:".
- Schleicher_ASW_24 moreGeneral "*Water ballast: ::::ASW 24B * Cockpit width: * Cockpit height: ASW 24E".
- Schleicher_K_10 moreGeneral "*Wing loading: 25.5 kg/m2".
- Schleicher_Ka_3 moreGeneral "*Wing loading: 19.5 kg/m2 maximum".
- Schneider_ES-49 moreGeneral "*'''Wing loading".
- Schneider_ES-54_Gnome moreGeneral "*Wing loading: 20.2 kg/m2".
- Schneider_ES-56_Nymph moreGeneral "*Wing loading: 23.8 kg/m2".
- Schneider_ES-57_Kingfisher moreGeneral "*Wing loading: 20.7 kg/m2".
- Schneider_ESG_31_Schlesierland moreGeneral "*Wing loading: 13.5 kg/m²".
- Schneider_Grunau_8 moreGeneral "* Wing loading: 16.35 kg/m²".
- Schneider_Moazagotl moreGeneral "*Wing loading: 13.5 kg/m² without ballast, 16.0 kg/m² ballasted".
- Schweizer_X-26_Frigate moreGeneral "Propeller: Ole Fahlin four-blade, 8 inch chord, fixed-pitch 100 inch diameter *Wing aspect ratio: 18 *Fuel Capacity: 20 gallons".
- Schweizer_X-26_Frigate moreGeneral "Wing aspect ratio: 18".
- Shenyang_J-11 moreGeneral "Fuel capacity: 9,400 kg internally".
- Shenyang_J-15 moreGeneral "444.0".
- Shenyang_J-6 moreGeneral "Fuel capacity: 1,800 kg".
- Shin_Meiwa_US-1A moreGeneral "plus 1× General Electric T58 gas turbine, 1,104 kW driving boundary layer control system".
- Short_Mayo_Composite moreGeneral "* Normal composite launch weight: 20,800 lb * Record composite launch weight: 26,800 lb".
- Short_Mayo_Composite moreGeneral "*Takeoff weight : 27,700 lb".
- Short_SB.1 moreGeneral "* Leading-edge sweep: 42.25°".
- Short_SB.5 moreGeneral "Fuel capacity: 300 Imp. gallons".
- Short_SC.1 moreGeneral "* Powerplant: ** Lift: 4× Rolls-Royce RB108 turbojets, 2,130 lbf each ** Forward flight: 1× Rolls-Royce RB108 turbojet, 2,130 lbf".
- Short_Sperrin moreGeneral "Fuel capacity: 6,200 gallons".
- Sikorsky_CH-148_Cyclone moreGeneral "Fuselage length: 56 ft 2 in * Fuselage width: 17 ft 3 in".
- Sikorsky_CH-53E_Super_Stallion moreGeneral "Rotor systems: 7 blades on main rotor, 4 blades on anti-torque tail rotor".
- Sikorsky_CH-53K_King_Stallion moreGeneral "Rotor systems: 7 blades on main rotor , 4 blades on tail rotor".
- Sikorsky_CH-53_Sea_Stallion moreGeneral "Width : 28 ft 4 in *Width : 15 ft 6 in *Rotor systems: 6 blades on main rotor".
- Sikorsky_Ilya_Muromets moreGeneral "Fuel and oil: 600 kg".
- Sikorsky_MH-53 moreGeneral "Rotor system: 6 blades on main rotor, 4 blades on tail rotor".
- Sikorsky_S-10 moreGeneral "Wing Load: 22kg/m²".
- Sikorsky_S-10 moreGeneral "Wing Load: 24.3kg/m²".
- Sikorsky_S-61R moreGeneral "Rotor system: 5 blades".
- Sikorsky_S-67_Blackhawk moreGeneral "Rotor system: 5 blades on main rotor, 5 blades on tail rotor * Fuselage length: * Fuselage height: * Stub wing span:".
- Sikorsky_S-69 moreGeneral "345".
- Sikorsky_S-69 moreGeneral "Rotor: 2 three-bladed co-axial, with 30 inch separation".
- Sikorsky_S-70 moreGeneral "Fuel, internal: 1,360 L * Auxiliary Fuel: 2x 700 L tanks internally, 1,705 L tank on each inboard pylon and 872 L tank on each outboard pylon, or 1,705 L tank on each pylon".
- Sikorsky_S-72 moreGeneral "* Take-off weight without auxiliary jets: 8,300 kg * Empty weight without auxiliary jets: 6,535 kg".
- Sikorsky_S-92 moreGeneral "Fuselage length: 56 ft 2 in *Fuselage width: 17 ft 3 in *Rotor systems: Main rotor has 4 blades. From the main gearbox a set of driveshafts connect to the tail gearbox to turn the 4-blade tail rotor. *Cabin dimensions: 20 ft long by 6.6 ft tall".