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Home > Grumman X-29


Grumman X-29
Description
RoleTechnology Demonstrator
Crew1
First Flight December 14, 1984
ManufacturerGrumman Aerospace Corporation
Dimensions
Length48 ft 1 in14.7 m
Wingspan27 ft 2 in8.8 m
Height14 ft 3 in4.3 m
Weights
Emptylbkg
Loadedlbkg
Maximum takeoff17,300 lb7,700 kg
Powerplant
Engines1x General Electric F404 turbofan
Thrust16,000 lb71.3 kN
Performance
Maximum speed1,200mph1,930km/h
Rangemileskm
Service ceiling55,000 ft16,800 m
Rate of climbft/minm/min
Wing loadinglb/ft²kg/m²
Thrust/Weight
Avionics
Avionics


The Grumman X-29 explored a number of new technologies, the most immediately obvious being the forward swept wings (FSW) and canard control surface. The inherent aerodynamic instability of this arrangement required the use of computerised fly-by-wire control, and advanced composite materials were needed to make the wing sufficiently rigid without being unacceptably heavy.

Two X-29As were built by Grumman Aerospace Corporation, and first flown in 1984. The two aircraft were made from existing Northrop F-5A Freedom Fighter airframes. The test program of the two planes continued for over a decade, and on December 13, 1985 one of them became the first FSW aircraft to fly supersonically in level flight.

The X-29A demonstrated excellent control and maneuvering qualities at an angle of attack up to 45 degrees.

The wing configuration made the craft inherently unstable. It could fly only with the constant corrections (up to 40 per second) provided by the computerised flight control system. The system was made up of three redundant digital computers backed up by three redundant analog computers. It was estimated that a total failure of the system was as unlikely as a mechanical failure in a normal airplane.

The first craft built is now on display in the USAF Museum.


1 Serial numbers


2 Also See

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