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A comparison of high cycle fatigue methodologiesTo evaluate alternate turbopump development (ATD) high cycle fatigue (HCF) methodology, a comparison was made with the space shuttle main engine (SSME) methodology. This report documents the comparison and evaluates ATD's HCF system.
Document ID
19930002960
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Herda, D. A. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:103601
NASA-TM-103601
Report Number: NAS 1.15:103601
Report Number: NASA-TM-103601
Accession Number
93N12148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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