File:Cold-Flow Propulsion Research Test - GPN-2000-000068.jpg
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DescriptionCold-Flow Propulsion Research Test - GPN-2000-000068.jpg |
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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Date | |||||||
Source | Great Images in NASA Description | ||||||
Author | NASA Terry Leibold | ||||||
Permission (Reusing this file) |
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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. This tag does not indicate the copyright status of the attached work. A normal copyright tag is still required. See Commons:Licensing. Other languages:
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current | 21:17, 8 April 2009 | 3,000 × 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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