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NASA NTRS · 19670005572

Mechanical Impact System Design for Advanced Spacecraft /MISDAS/

Bernstein, A. I.

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Abstract

Radial skid and six segment heat shield concepts evaluated for Mechanical Impact System Design for Advanced Spacecraft /MISDAS/

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HEAT SHIELD SKID LANDING IMPACT LANDING SYSTEM

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Bernstein, A. I.. 1966-05-13. Mechanical Impact System Design for Advanced Spacecraft /MISDAS/. https://ntrs.nasa.gov/citations/19670005572

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