Studies of hypervelocity impact phenomena as applied to the protection of spacecraft operating in the MMOD environment
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Published:2017
Issue:
Volume:204
Page:4-42
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ISSN:1877-7058
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Container-title:Procedia Engineering
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language:en
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Short-container-title:Procedia Engineering
Author:
Schonberg William P.
Subject
Applied Mathematics
Reference70 articles.
1. “Meteorites and space travel”;Whipple;Astronomical Journal,1947
2. Schonberg, W.P., “The Development of Ballistic Limit Equations for Dual-Wall Spacecraft Shielding: A Concise History and Suggestions for Future Development”, 49th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, AIAA Paper No. 2008-1966, Chicago, IL, April, 2008.
3. "Hypervelocity Impact Penetration Phenomena in Aluminum Space Structures";Schonberg;Journal of Aerospace Engineering,1990
4. "Penetration and Ricochet Phenomena in Multi-Sheet Structures under Oblique Hypervelocity Impact";Schonberg;AIAA Journal,1989
5. "Characterizing Secondary Debris Impact Ejecta";Schonberg;International Journal of Impact Engineering,2001
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