NASA NTRS · 19850003067
Materials properties, loads, and stress analysis, Spartan REM: Appendix A
Abstract
The 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.
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Marlowe, D. S., West, E. J.. 1984-06-19. Materials properties, loads, and stress analysis, Spartan REM: Appendix A. https://ntrs.nasa.gov/citations/19850003067
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