NASA NTRS · 20110011932
Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure
Abstract
A 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.
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Zwitter, James G., Adams, Marc A.. 2011-04-01. Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure. https://ntrs.nasa.gov/citations/20110011932
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