NASA NTRS · 19670005559
Mechanical Impact System Design for Advanced Spacecraft /MISDAS/. Phase I - Design Concept Selection
Abstract
Mechanical impact system for earth landing of Apollo command module
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Bernstein, A. I.. 1965-09-20. Mechanical Impact System Design for Advanced Spacecraft /MISDAS/. Phase I - Design Concept Selection. https://ntrs.nasa.gov/citations/19670005559
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