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Grumman Aerospace Grumman X-29 Demo 

A Grumman X-29 in flight
Role Experimental aircraft
National origin United States
Manufacturer Grumman
First flight 14 December 1984
Status Retired
Primary users United States Air Force
NASA
Number built 2
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History Grumman X-29 American experimental aircraft,
 that tested a forward-swept wing

Operational history

The first X-29 took its maiden flight on 14 December 1984 from Edwards AFB piloted by Grumman's Chief Test Pilot Chuck Sewell. The X-29 was the third forward-swept wing jet-powered aircraft design to fly; the other two were the German Junkers Ju 287 (1944) and the HFB-320 Hansa Jet (1964). On 13 December 1985, an X-29 became the first forward-swept wing aircraft to fly at supersonic speed in level flight.

Grumman X-29A at the National Museum of the United States Air Force
Grumman X-29 at Edwards Air Force Base

The X-29 began a NASA test program four months after its first flight. The X-29 proved reliable, and by August 1986 was flying research missions of over three hours involving multiple flights. The first X-29 was not equipped with a spin recovery parachute, as flight tests were planned to avoid maneuvers that could result in departure from controlled flight, such as a spin. The second X-29 was given such a parachute and was involved in high angle-of-attack testing. X-29 number two was maneuverable up to an angle of attack of about 25 degrees with a maximum angle of 67° reached in a momentary pitch-up maneuver.

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Take off Distance

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Aircraft Speed

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Max Crew

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Grumman Aerospace Corporation,

Grumman Aerospace Corporation
Grumman X-29 American experimental aircraft that tested a forward-swept wing

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General characteristics

  • Crew: 1
  • Capacity: 4,000 lb (1,814 kg) payload
  • Length: 53 ft 11.25 in (16.4402 m) including nose probe
  • 48 ft 1 in (15 m) fuselage only
    • Wingspan: 27 ft 2.5 in (8.293 m)
    • Height: 14 ft 3.5 in (4.356 m)
    • Wing area: 188.84 sq ft (17.544 m2)
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Powerplant

  • Empty weight:  (6,260 kg)
  • Max takeoff weight: (8,074 kg)
  • Fuel capacity:  (1,804 kg) in two fuselage bladder tanks and two strake integral tanks
  • Powerplant: 1 × General Electric F404-GE-400 afterburning turbofan engine, 16,000 lbf (71 kN) with afterburner
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Specifications

  • Maximum speed: 956 kn (1,100 mph, 1,771 km/h) at 33,000 ft (10,058 m)
  • Maximum speed: Mach 1.6
  • Range: 350 nmi (400 mi, 650 km)
  • Service ceiling: 55,000 ft (17,000 m)
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Avionics

    • Litton LR-80 AHRS
    • Magnavox AN/ARC-164 UHF
    • Teledyne RT-1063B/APX-101V IFF/SIF
    • Honeywell triple redundant fly-by-wire FCS
Special Links Grumman Aerospace Corporation,  Grumman X-29 American experimental aircraft that tested a forward-swept wing  

Links to Youtube & Others

wo X-29As were built by Grumman after the proposal had been chosen over a competing one involving a General Dynamics F-16 Fighting Falcon. The X-29 design made use of the forward fuselage and nose landing gear from two existing F-5A Freedom Fighter airframes (63-8372 became 82-0003 and 65-10573 became 82-0049).

Grumman X-29 experimental aircraft

The X-29 is described as a three surface aircraft, with canards, forward-swept wings, and aft strake control surfaces,

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Youtube Link

The high pitch instability of the airframe led to wide predictions of extreme maneuverability. This perception has held up in the years following the end of flight tests.

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