Rockwell XFV-12
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The Rockwell XFV-12 was a prototype supersonic
United States Navy The United States Navy (USN) is the maritime service branch of the United States Armed Forces and one of the eight uniformed services of the United States. It is the largest and most powerful navy in the world, with the estimated tonnage ...
fighter which was built in 1977. The XFV-12 design attempted to combine the Mach 2 speed and
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armament of the
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in a
VTOL A vertical take-off and landing (VTOL) aircraft is one that can take off and land vertically without relying on a runway. This classification can include a variety of types of aircraft including helicopters as well as thrust-vectoring fixed-win ...
(vertical takeoff and landing) fighter for the small
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which was under study at the time. On paper, it looked superior to the subsonic
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attack fighter. However it was unable to demonstrate an untethered vertical takeoff and its inability to meet performance requirements terminated the program.


Design and development

In 1972, the Navy issued a request for proposals for a next generation supersonic V/STOL fighter/attack aircraft. Rockwell's design with the XFV-12 won against
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's proposal with the
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. The XFV-12A, despite its concept being considered risky compared to that of the Harrier, was selected for development. To reduce costs, the nose from a
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and intakes from the F-4 were used. Engine rig testing began in 1974. Free-flight model tests conducted at the
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full-scale wind tunnel showed the projected thrust augmentation levels were highly optimistic, and that the aircraft would most likely be incapable of vertical flight on the thrust available, while the design remained suitable for conventional flight. The XFV-12 used a thrust augmented wing concept in which exhaust would be directed through spaces in a wing opened up like
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to increase available lift, somewhat like Lockheed's unsuccessful
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. The 30,000 lbf (130 kN)-class afterburning
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engine had enough thrust to lift the weight of the 20,000 lb (9,072 kg) aircraft. It was modified to further increase thrust for vertical lift. The rear engine exhaust was closed and the gases redirected through ducts to ejector nozzles in the wings and canards for vertical lift.


Operational history

Ground testing of the XFV-12A began in July 1977, and the aircraft was officially rolled out at the Rockwell International facility in
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on 26 August. Due to increasing costs, construction of the second prototype was abandoned. Tethered hover tests were conducted in 1978. Over the course of six months, it was determined that the XFV-12A design suffered from major deficiencies with regard to vertical flight, especially a lack of sufficient vertical thrust. Lab tests showed 55% thrust augmentation should be expected; however, differences in the scaled-up system dropped augmentation levels to 19% for the wing and a mere 6% in the canard. While the augmenters did work as expected, the extensive ducting of the propulsion system degraded thrust, and in the end the
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was such that the engine was capable of vertically lifting only 75% of the weight of the aircraft in which it was mounted. Following the tests, and with the program suffering from cost overruns, the Navy decided the XFV-12A was not worth further development, and cancelled the project in 1981. The October 6, 1975 issue of ''
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'' published an article about the Rockwell NA-382 which was an even more ambitious proposal to the Marine Corps to fit a similar wing to the
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, but the plan never made it off the drawing board. Of the two prototypes built, only one was completed, while the second prototype was cancelled. The
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eventually adopted the subsonic British-designed Harrier, the only truly successful
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design of the 1960s. Its replacement, the
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, uses a shaft-driven fan and a swivelling rear nozzle to achieve vertical landing. It is designed for supersonic and vertical flight with performance just over Mach 1.5 with weapons and range comparable to the older F-4 and F-18.


Surviving aircraft

Following program cancellation, the aircraft was disassembled and the cockpit section of the fuselage was stored at NASA's
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in Sandusky, Ohio. As of May 2012, a group of high school students at the
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, with guidance from NASA contractor personnel, were to restore the fuselage for use as a museum display.


Specifications


See also


References

;Notes ;Bibliography *Buttler, Tony. ''American Secret Projects, Fighters & Interceptors 1945-1978''. Hinckley, UK: Midland Publishing. 2007. . * * *


External links


Line illustration of the Rockwell XFV-12Illustration of XFV-12 engine airflow
{{USAF fighters Cancelled military aircraft projects of the United States Canard aircraft Carrier-based aircraft FV-12 Rockwell FV-12 V/STOL aircraft by thrust vectoring Single-engined jet aircraft