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Description X-31 Aircraft Specifications, X-31 3-side view Designed and constructed as a demonstrator aircraft by Rockwell International Corporation's North American Aircraft and Deutsche Aerospace, the X-31 had a wing span of 23.83 feet. The fuselage length was 43.33 feet. The X-31 was powered by a single General Electric F404-GE-400 turbofan engine, producing 16,000 pounds of thrust in afterburner. Typical takeoff weight of the X-31 was 16,100 pounds including 4,100 pounds of fuel. The X-31 design speed was Mach 0.9 with an altitude capability of 40,000 feet. For specific tests to determine thrust vectoring effectiveness at supersonic speeds the aircraft was flown to Mach 1.28 at an altitude of 35,000 feet.
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This is a retouched picture, which means that it has been digitally altered from its original version. Modifications: zwektoryzowano. The original can be viewed here: Rockwell-MBB X-31 3-view line drawing.jpg: . Modifications made by Krzysztof Zajączkowski.

Licensing

Public domain This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)
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This image is a derivative work of the following images:

  • File:111373main_X-31_3-view.jpg licensed with PD-USGov-NASA
    • 2005-12-04T10:38:21Z Stahlkocher 330x245 (40885 Bytes) NASA X-31 3-side view :Source:Nasa {{PD}} [[category:Experimental aircraft]] [[category:Aircraft line drawings]]

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28 August 2010

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current07:38, 28 August 2010Thumbnail for version as of 07:38, 28 August 2010330 × 245 (49 KB)Malyszkz{{Information |Description='''X-31 Aircraft Specifications, X-31 3-side view''' Designed and constructed as a demonstrator aircraft by Rockwell International Corporation's North American Aircraft and Deutsche Aerospace, the X-31 had a wing span of 23.83

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