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A Regeneratively-Cooled Thrust Chamber for the Fastrac EngineThis document consists of presentation slides about the development of the regeneratively cooled thrust chamber for the Fastrac engine. The Fastrac engine was originally developed to demonstrate low cost design and fabrication methods. It was intended to be used in an expendable booster. The regen thrust chamber enables a more cost efficient test program. Using the low cost design and fabrication methodology designed for the 12K regeneratively cooled chamber, the contractor designed, developed and fabricated a regeneratively cooled thrust chamber for the Fastrac engine.
Document ID
20000112951
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Brown, Kendall
(NASA Marshall Space Flight Center Huntsville, AL United States)
Sparks, Dave
(NASA Marshall Space Flight Center Huntsville, AL United States)
Woodcock, Gordon
(Space America, Inc. United States)
Jim Turner
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Joint Propulsion
Location: Huntsville, Al
Country: United States
Start Date: July 17, 2000
End Date: July 19, 2000
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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