Global Aircraft -- X-29 FSW
 
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X-29 FSW Specifications
Primary Function: Experimental Aircraft
Contractor: Grumman
Crew: One
Unit Cost: N/A
Powerplant
  One General Electric F404-GE-400 at 16,000 lb of thrust
Dimensions
Length: 48.1 feet
Wingspan: 27.2 feet
Height: 14 feet
Weights
Empty: 13,600 lb
Maximum Takeoff: 17,600 lb
Performance
Speed: Mach 1.6 (1,120mph)
Ceiling: 50,000 feet
Range: N/A
Armament
  N/A


X-29 FSW Achievements
  • Studies from the X-29 showed that forward swept wings, coupled with movable canards, gave pilots excellent control response.


X-29 FSW Background
 

   Two X-29 Forward Swept Wing aircraft were built as advanced concepts and technology demonstrators. The test program was conducted from 1984 to 1992 and provided an ample supply of engineering information which can be used for the design and development of future aircraft.

   The X-29 featured forward swept wings planted well in the back of the fuselage, and canards to control pitch and acted as horizontal stabilizers. This new wing design proved exceptional maneuverability, a light structure, and supersonic performance. The test results of this design showed excellent control response at angles of attack up to 45 degrees. During its life, the X-29 aircraft were flown on 422 research missions. Including non-research flights, the X-29 aircraft flew 436 missions total.

Summary Copyright © Charles M (JetWhiz)



X-29 FSW Photos
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X-29 FSW





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