| タイトル | Analysis of reentry into the White Sands Missile Range (WSMR) for the LifeSat mission |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930015528 |
| 著者（英） | Cooley, J.; Snow, F.; Roszman, L.; Hametz, M. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1993-02-01 |
| 言語 | eng |
| 内容記述 | This study investigates the reentry of the LifeSat vehicles into the WSMR. The LifeSat mission consists of two reusable reentry satellites, each carrying a removable payload module, which scientists will use to study long-term effects of microgravity, Van Allen belt radiation, and galactic cosmic rays on living organisms. A series of missions is planned for both low-Earth circular orbits and highly elliptic orbits. To recover the payload module with the specimens intact, a soft parachute landing and recovery at the WSMR is planned. This analysis examines operational issues surrounding the reentry scenario to assess the feasibility of the reentry. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 93N24717 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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