Image:111373main X-31 3-view.jpg

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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.
Source
This image or video was catalogued by Dryden Flight Research Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: X-31 Fact Sheet.
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Date

October 27, 2007
Author

Marty Curry, DFRC
Permission
(Reusing this image)
Public domain
 This file is in the public domain because it was created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (NASA copyright policy page or JPL Image Use Policy).

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Date et heureDimensionsUtilisateurCommentaire
actuel4 décembre 2005 à 12:38330×245 (40 Kio)Stahlkocher (NASA X-31 3-side view :Source:Nasa {{PD}} category:Experimental aircraft category:Aircraft line drawings)

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Métadonnées

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Résolution horizontale 72 dpi
Résolution verticale 72 dpi
Logiciel utilisé Adobe Photoshop CS Macintosh
Date de modification 23 mars 2005 à 07:47
Espace colorimétrique 65535