| タイトル | Orbital debris environment for spacecraft designed to operate in low Earth orbit |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890013267 |
| 著者（英） | Reynolds, Robert C.; Anz-Meador, Phillip D.; Kessler, Donald J. |
| 著者所属（英） | NASA Johnson Space Center|Lockheed Engineering and Sciences Co. |
| 発行日 | 1988-09-01 |
| 言語 | eng |
| 内容記述 | The orbital debris environment model is intended to be used by the spacecraft community for the design and operation of spacecraft in low Earth orbit. This environment, when combined with material-dependent impact tests and spacecraft failure analysis, is intended to be used to evaluate spacecraft vulnerability, reliability, and shielding requirements. The environment represents a compromise between existing data to measure the environment, modeling of this data to predict the future environment, the uncertainty in both measurements and modeling, and the need to describe the environment so that various options concerning spacecraft design and operations can be easily evaluated. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 89N22638
NASA-TM-100471
NAS 1.15:100471 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/142222 |
