McDonnell Douglas X-36

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McDonnell-Douglas X-36
Description
Role Tailless Fighter Agility Research Aircraft
Crew 0
First Flight May 17, 1997
Manufacturer McDonnell Douglas
Dimensions
Length 19 ft 5.8 m
Wingspan 10 ft 3.0 m
Height 3 ft 0.9 m
Wing area ft²
Weights
Empty lb kg
Loaded lb kg
Maximum takeoff 1,250 lb 550 kg
Powerplant
Engines Williams International F112 turbofan
Thrust 700 lbf 3.1 kN
Performance
Maximum speed 234 mph 375 km/h
Range miles km
Service ceiling 20,000 ft 6,000 m
Rate of climb ft/min m/min
Wing loading lb/ft² kg/m²
Thrust/Weight 0.56 lbf/lb 5.5 N/kg
Power/Mass hp/lb kW/kg
Avionics
Avionics

The McDonnell Douglas X-36 Tailless Fighter Agility Research Aircraft was a subscale prototype jet designed to fly without the traditional tail surfaces common on most aircraft.

For control, a canard forward of the wing was used as well as split ailerons and an advanced thrust vectoring nozzle for directional control. The X-36 was unstable in both pitch and yaw axes, so an advanced digital fly-by-wire control system was put in place to stabilize the aircraft.

The X-36 was built to approximately one-quarter scale of a possible fighter aircraft, and controlled by a pilot in a ground station virtual cockpit with a view provided by a video camera mounted in the nose of the aircraft.

First flown on May 17, 1997, it made 31 successful research flights. It handled very well, and the program is reported to have met or exceeded all project goals.

The aircraft is sometimes referred to as the Boeing X-36 as the test program was still in progress when McDonnell Douglas merged with the Boeing Company. In the adjoining photograph it is carrying Boeing markings.

This aircraft was inducted into the United States Air Force Museum at Wright-Patterson Air Force Base on July 16, 2003.

See also

Related content
Related Development

X-45

Similar Aircraft
Designation Series

X33 - X-34 - X-35 - X-36 - X-37 - X-38 - X-39

Related Lists

List of experimental aircraft