McDonnell Douglas X-36

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McDonnell-Douglas X-36
300px
Description
RoleTailless Fighter Agility Research Aircraft
Crew0
First FlightMay 17, 1997
ManufacturerMcDonnell Douglas
Dimensions
Length19 ft5.8 m
Wingspan10 ft3.0 m
Height3 ft0.9 m
Wing areaft²
Weights
Emptylbkg
Loadedlbkg
Maximum takeoff1,250 lb550 kg
Powerplant
EnginesWilliams International F112 turbofan
Thrust700 lbf3.1 kN
Performance
Maximum speed234 mph375 km/h
Rangemileskm
Service ceiling20,000 ft6,000 m
Rate of climbft/minm/min
Wing loadinglb/ft²kg/m²
Thrust/Weight0.56 lbf/lb5.5 N/kg
Power/Masshp/lbkW/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.

Also See

This article or image contains materials that originally came from a NASA website. All NASA information is in the public domain, with the exception of the usage-restricted NASA logo. See here (http://www.jsc.nasa.gov/policies.html#Guidelines) for more information.


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Designation Series

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

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