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Space Shuttle Main Engine structural analysis and data reduction/evaluation. Volume 5: Main Injector LOX Inlet analysisThe analysis performed on the Main Injector LOX Inlet Assembly located on the Space Shuttle Main Engine is summarized. An ANSYS finite element model of the inlet assemably was built and executed. Static stress analysis was also performed.
Document ID
19890018326
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Violett, Rebeca S. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-183668
LMSC-HEC-TR-F268584-VOL-5
NAS 1.26:183668
Accession Number
89N27697
Funding Number(s)
CONTRACT_GRANT: NAS8-37282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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