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Meteoroid/orbital debris shield engineering development practice and procedure
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zwitter, James G. Adams, Marc A. |
| Copyright Year | 2011 |
| Description | 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. |
| File Size | 173610 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110011932 |
| Archival Resource Key | ark:/13960/t0ns5r49r |
| Language | English |
| Publisher Date | 2011-04-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Spacecraft Shielding Space Debris Spacecraft Components Probability Theory Micrometeoroids Computerized Simulation Monte Carlo Method Spacecraft Design Hypervelocity Impact Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
