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Space Shuttle Main Engine structural analysis and data reduction/evaluation. Volume 3A: High pressure oxidizer turbo-pump preburner pump housing stress analysis reportThe model generation and structural analysis performed for the High Pressure Oxidizer Turbopump (HPOTP) preburner pump volute housing located on the main pump end of the HPOTP in the space shuttle main engine are summarized. An ANSYS finite element model of the volute housing was built and executed. A static structural analysis was performed on the Engineering Analysis and Data System (EADS) Cray-XMP supercomputer
Document ID
19890018323
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shannon, Robert V., Jr.
(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-183665
NAS 1.26:183665
LMSC-HEC-TR-F268584-VOL-3A
Report Number: NASA-CR-183665
Report Number: NAS 1.26:183665
Report Number: LMSC-HEC-TR-F268584-VOL-3A
Accession Number
89N27694
Funding Number(s)
CONTRACT_GRANT: NAS8-37282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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