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Materials properties, loads, and stress analysis, Spartan REM: Appendix AThe mechanical properties, load tests, and stress analysis of the Spartan Release Engagement Mechanism (REM) is presented. The fracture properties of the components of the unit are also discussed. Detailed engineering drawings are included.
Document ID
19850003067
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Marlowe, D. S. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
West, E. J. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
June 19, 1984
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:171092
LMSC-HREC-PR-D951498-A
NASA-CR-171092
Report Number: NAS 1.26:171092
Report Number: LMSC-HREC-PR-D951498-A
Report Number: NASA-CR-171092
Accession Number
85N11375
Funding Number(s)
CONTRACT_GRANT: NAS8-35599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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