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X-35 Joint Strike Fighter
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Photo: Robert Deering 10/23/2006 Smithsonian National Air and Space Museum Dulles International Airport (IAD) Chantilly, Virginia |
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This aircraft is
the first X-35 ever built. It was originally
the X-35A and was modified to include the
lift-fan engine for testing of the STOVL
concept. Among its many test records, this
aircraft was the first in history to achieve
a short takeoff, level supersonic dash, and
vertical landing in a single flight. It is
also the first aircraft to fly using a
shaft-driven lift-fan propulsion system. The
X-35B flight test program was one of the
shortest, most effective in history, lasting
from June 23, 2001 to August 6, 2001.
The lift-fan propulsion system is now displayed next to the X-35B at the Steven F. Udvar-Hazy Center near Dulles Airport. On July 7, 2006, the production model F-35 was officially named F-35 Lightning II by T. Michael Moseley, Chief of Staff USAF. Dimensions: Wing span: 10.05 m (33 ft 0 in) Length: 15.47 m (50 ft 9 in) Height: approximately 5 m (15 ft 0 in) Weight: approximately 35,000 lb. Materials: Composite material aircraft skin, alternating steel and titanium spars. Single-engine, single-seat configuration includes lift-fan and steering bars for vertical flight. Physical Description: Short takeoff/vertical landing variant to be used by U.S. Air Force, U.S. Marines and the United Kingdom, equipped with a shaft-driven lift fan propulsion system which enables the aircraft to take off from a short runway or small aircraft carrier and to land vertically. Engine: Pratt & Whitney JSF 119-PW-611 turbofan deflects thrust downward for short takeoff/vertical landing capability. The Air Force and Navy versions use a thrust-vectoring exhaust nozzle. The Marine Corps and Royal Air Force/Navy version has a swivel-duct nozzle; an engine-driven fan behind the cockpit and air-reaction control valves in the wings to provide stability at low speeds. Other major subcontractors are Rolls Royce and BAE.
Source:
Smithsonian National Air & Space Museum |
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