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Space Shuttle main engine powerhead structural modeling, stress and fatigue life analysis. Volume 1: Gasdynamic environment of the SSME HPFTP and HPOTP turbinesGasdynamic analysis for the turbine blades and nozzle vanes, HPFTP turbine analysis, and HPOTP turbine analysis are provided.
Document ID
19840012567
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hammett, J. C. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Hayes, C. H. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Price, J. M. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Robinson, J. K. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Teal, G. A. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Thomson, J. M. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Tilley, D. M. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Welch, C. T. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:170999
NASA-CR-170999
LMSC-HREC-TR-D867333-I
Accession Number
84N20635
Funding Number(s)
CONTRACT_GRANT: NAS8-34978
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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