2013 sea trials and shows the amazing hovering F-35B making its first vertical at-sea night landing on the USS WASP. F-35B STOVL F-35C CATOBAR.
Simpleplanes Lockheed Martin F 35b
39700 lb After burner not used in STOVL mode.
F-35b stovl specifications. The F-35B features a wingspan of 35 feet a fuselage length of 505 feet and a wing area of 460 square feet. Specifications Lockheed Martin F-35B Lightning. An ability to produce 39800lbs of thrust minus 29735 lbs gross weight and 3000 lbs of thrust to safely maneuver the aircraft equals 7065 l.
About Mach 15. One Pratt. F-35B - STOVL variant with Vertical Flight System VFS.
The F-35B Short take-off and landing for US Marine Corps is the first aircraft in history to combine stealth with short takeoffvertical landing capability and supersonic speed. 39700 lb After burner not used in STOVL mode. The F-35B is the short takeoff and vertical landing STOVL variant of the aircraft.
35ft 1070m Wing area. 514 ft 157 m 513 ft 156 m 515 ft 157 m Wingspan. STOVL capability gives the F-35B the unique capability to operate from a variety of ships roads and austere bases near frontline combat zones greatly enhancing sortie generation rates.
LiftFan Two-stage contra-rotating hollow titanium blisk fan of 50 inches 13 m diameter. The counter-swivel lifting fan established by Rolls-Royce Defense can produce thrust of more than 20000 lb. Doors mounted above and below the fan are vertically open when the fins spin up to provide vertical lift.
Equipped with a lift fan design capable of producing 39800 lbs of vertical lift at sea level on a tropical day. Reduced fuel stores reducing operational range. Folding wingtips for shipborne storage.
Increased wing and tail surfaces for improved low-and-slow handling. Takeoffs and landing with vertical flight systems are by far the riskiest and in the end a decisive factor in design. On the F-35B the engine is coupled with a drive fan system which is driven by a shaft for the STOVL drive.
F-35B Short-takeoff and vertical-landing STOVL mainly for the British Government F-35C Carrier-based CV for US. Similar in size to the A variant the B sacrifices some fuel volume to make room for the vertical flight system. 18250 lb 8280 kg 13500 lb 6125 kg 19750 lb 8860 kg.
460sqft 4270m2 Maximum take-off weight. Naval Forces Engines selected for this aircraft includes the Pratt and Whitney F135 and General Electric Rolls-Royce F136 though the STOVL versions with both the engines will use the highly advanced Rolls-Royce. Twin-wheeled nose landing gear leg.
Reduced G-stress levels of airframe. Vertical Thrust STOVL na. The jet measures 156m 512ft in overall length has a wingspan of 107m 35ft and a height of 436m 143ft.
35 ft 107 m 35 ft 107 m 43 ft 131 m Wing Area. Shaft-driven lift fan augments engines lifting force. Internal fuel is listed at 13326lbs.
It is reported that Lockheed consulted with people at the Russian Yakovlev aircraft firm and purchased some relatable data. The counter-swivel lifting fan developed by Rolls-Royce Defense can produce thrust of more than 20000 lb. Uppermost fan fitted with variable inlet guide vanes.
Below the videos is a photo of the F35B in STOVL mode with specs. Its top speed comes in at 16 Mach or 1200mph that is 16 times the speed of sound. Max Level Speed at altitude.
Specifications LiftSystem Main engine Pratt Whitney F135 17600 pounds-force 78 kN dry thrust. 14ft 3½in 436m Wingspan. Increasingly modern security challenges require wider distribution of forces and capabilities across a range of scenarios.
The jets maximum thrust tops 40000lbs it has an amazing range of 900 nautical miles and a combat radius of 833km. This distinction gives the F-35B the unique ability to operate from small ships roads and austere bases. Shaft-driven lift fan augments engines lifting force.
Capable of generating more than 20000 pounds-force 89 kN cold thrust. 460 ft² 427 m² 460 ft² 427 m² 668 ft² 621 m² Empty weight. Theres also a quick takeoff shown.
The unmatched basing of the F-35B ashore and afloat provides more employment flexibility in any. F-35C - Navalized fixed-wing F-35A. 29300 lb 13300 kg 32300 lb 14700 kg 34800 lb 15800 kg Internal fuel.
Vertical Thrust STOVL na. On the F-35B the engine is paired with a drive fan system which is driven by a shaft for the STOVL drive. F-35B STOVL.
Doors mounted above and below the fan are vertically open when the fins spin up to provide vertical lift. 51ft 2¼in 1560m Height.
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