Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure
TBMG-9613
04/01/2011
- 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.
- Citation
- "Meteoroid/Orbital Debris Shield Engineering Development Practice and Procedure," Mobility Engineering, April 1, 2011.