File:Oxidizer preburner.jpg

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Description The oxidizer preburner — intended to initiate the fuel combustion process for the Integrated Powerhead Demonstrator — was designed and tested for NASA and the Air Force by Aerojet Corp. of Sacramento, Calif., facilities. The preburner generates oxygen-rich steam for use by the oxygen turbopump's turbine. Testing of the preburner was completed in October — a critical milestone in the development of innovative engine systems that could, within decades, power a new generation of American space launch vehicles. (Aerojet Corp.)
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Source http://www.nasa.gov/centers/marshall/images/content/98907main_Aerojet-IPD-preburner.jpg
Author nasa
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Other versions http://www.nasa.gov/centers/marshall/multimedia/photos/2003/photos03-203_prt.htm
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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current10:57, 14 February 2008Thumbnail for version as of 10:57, 14 February 20081,500 × 1,033 (1.19 MB)Emesee (talk | contribs){{Information |Description=The oxidizer preburner — intended to initiate the fuel combustion process for the Integrated Powerhead Demonstrator — was designed and tested for NASA and the Air Force by Aerojet Corp. of Sacramento, Calif., facilities. The

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