File:Cold-Flow Propulsion Research Test - GPN-2000-000068.jpg

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English: An engineer at the Marshall Space Flight Center (MSFC) Wind Tunnel Facility uses lasers to measure the velocity and gradient distortion across an eight inch curved pipe with joints and turning valves during a cold-flow propulsion research test; simulating the conditions found in the X-33's hydrogen feedline. Lasers are used because they are non-intrusive and do not disturb the flow like a probe would. The feedline supplies propellants to the turbo pump. The purpose of this project was to design the feedline to provide uniform flow into the turbo pump.
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Source Great Images in NASA Description
Author NASA Terry Leibold
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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 or video was catalogued by Marshall Space Flight Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: GPN-2000-000068 and Alternate ID: MSFC-9712449.

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current21:17, 8 April 2009Thumbnail for version as of 21:17, 8 April 20093,000 × 2,192 (4.38 MB)BotMultichillT (talk | contribs){{Information |Description={{en|1=An engineer at the Marshall Space Flight Center (MSFC) Wind Tunnel Facility uses lasers to measure the velocity and gradient distortion across an eight inch curved pipe with joints and turning valves during a cold-flow pr

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