X-31 Thrust Vectoring Fighter

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The purpose of the X-31 was to develop methods of achieving a high degree of maneuverablity at high speed. In high speed flight, the aircraft becomes more sluggish and hard to control due to the hundreds of pounds of pressure from the air hitting the control surfaces. This aircraft uses thrust vectoring in the tailpipe of the engine, enabling post-stall maneuvers as well as a higher degree of maneuverability at high speed. The X-31 has already been developed as an experimental aircraft, but the US is thinking about using it for a fighter.

 

Specs on the X-31

COUNTRY: USA, Germany
MANUFACTURER: Rockwell, MBB
MODEL: X-31A
ENGINE: One General Electric F404 turbofan engine
DIMENSIONS: Wingspan: 22.8'; Lt: 42.5'; Ht: 13.4'
WEIGHT: Gross: 13,968 lb; empty: 10,212 lb.
PERFORMANCE: Max speed: Mach 1.2; max alt: 50,000' approx.
WHERE BUILT: El Segundo, California; and Munchen, Germany
FIRST FLIGHT: October 11, 1990

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