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Space Shuttle Main Engine structural analysis and data reduction/evaluation. Volume 4: High pressure fuel turbo-pump inlet housing analysisThe analysis performed on the Space Shuttle Main Engine (SSME) High Pressure Fuel Turbopump (HPFTP) inlet housings is summarized. Three DIAL finite element models were build to aid in assessing the structural life of the welds and fillets at the vanes. Complete results are given.
Document ID
19890018325
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pool, Kirby V. (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
NAS 1.26:183667
NASA-CR-183667
LMSC-HEC-TR-F268584-VOL-4
Report Number: NAS 1.26:183667
Report Number: NASA-CR-183667
Report Number: LMSC-HEC-TR-F268584-VOL-4
Accession Number
89N27696
Funding Number(s)
CONTRACT_GRANT: NAS8-37282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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