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Space Shuttle main engine, powerhead structural modeling, stress and fatigue life analysis. Volume 4: Summary of investigation of unscheduled events and special tasksLow pressure fuel turbopump turbine labyrinth send tip rubbing analysis, gas dynamic analysis, and HPFTP blade crack and blade impact are presented.
Document ID
19840012570
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Robinson, J. K. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Teal, G. A. (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 1.26:171002
NASA-CR-171002
LMSC-HREC-TR-D867333-IV
Accession Number
84N20638
Funding Number(s)
CONTRACT_GRANT: NAS8-34978
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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