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Meteoroid/Orbital Debris Shield Engineering Development Practice and ProcedureA document describes a series of models created for the determination of the probability of survival of critical spacecraft components from particle strike damage caused by hypervelocity impact of meteoroids and/or orbital debris. These models were integrated with both shield design and hypervelocity impact testing to develop adequate protection of said components to meet mission survivability requirements.
Document ID
20110011932
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Zwitter, James G.
(California Inst. of Tech. Pasadena, CA, United States)
Adams, Marc A.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2011
Publication Information
Publication: NASA Tech Briefs, April 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NPO-46082
Distribution Limits
Public
Copyright
Public Use Permitted.
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