Magazine Article

Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure

TBMG-9613

04/01/2011

Abstract
Content

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 hyper-velocity 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.

Meta TagsDetails
Citation
"Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure," Mobility Engineering, April 1, 2011.
Additional Details
Publisher
Published
Apr 1, 2011
Product Code
TBMG-9613
Content Type
Magazine Article
Language
English