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Methodology for Identifying Key Parameters Affecting Reusability for Liquid Rocket EnginesTo use statistical techniques to identify which parameters are tightly correlated with increasing the reusability of liquid rocket engine hardware.




Document ID
20190027441
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Askins, Bruce (NASA Marshall Space Flight Center Huntsville, AL, United States)
Childress-Thompson, Rhonda (Alabama Univ. Huntsville, AL, United States)
Date Acquired
July 17, 2019
Publication Date
June 3, 2019
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M19-7435
Report Number: M19-7435
Meeting Information
Meeting: JANNAF Propulsion Meeting (JPM)
Location: Dayton, OH
Country: United States
Start Date: June 3, 2019
End Date: June 7, 2019
Sponsors: NASA Headquarters, Department of the Army, Department of the Air Force, Department of the Navy
Distribution Limits
Public
Copyright
Public Use Permitted.

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