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Rapid Vacuum Plasma Spray (VPS) Closeout of Liquid Rocket Engine Combustion Chamber Cooling Channels for Both Time and Cost SavingsThis viewgraph presentation describes the Rapid Vacuum Plasma Spray (VPS) and its rapid closeout of combustion chamber cooling channels for reduced time and reduced costs.
Document ID
20090028729
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Holmes, Richard R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Elam, Sandra K. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Power, Christopher A. (Genie Products, Inc. United States)
Date Acquired
August 24, 2013
Publication Date
June 22, 2009
Subject Category
Mechanical Engineering
Report/Patent Number
M09-0531
Report Number: M09-0531
Meeting Information
Meeting: National Space and Missile Materials Symposium
Location: Henderson, NV
Country: United States
Start Date: June 22, 2009
End Date: June 25, 2009
Distribution Limits
Public
Copyright
Public Use Permitted.

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