| タイトル | Thermal design and analysis in the Orbiter bay |
| 著者（英） | Coyle, M. J.; Humphries, W. R. |
| 著者所属（英） | NASA Marshall Space Flight Center|NASA Goddard Space Flight Center |
| 発行日 | 1983-01-01 |
| 言語 | eng |
| 内容記述 | Thermal design and integration of payloads located in the Orbiter bay are addressed. Methods used to satisfy equipment thermal requirements are discussed with particular emphasis on passive thermal control. Both fixed and tiltable payload configurations are covered. Design methodology, integration techniques, constraints and mission peculiar requirements are presented. Past and future Spacelab missions, including those utilizing the instrument pointing system are of special interest. The OSS-1 payload flown on STS-3 is presented in some detail. Design concepts for the 'all-up' thermal modeling techniques for this payload are discussed. A brief summary of orbital results for OSS-1 are given. Finally, as a special topic, a low power independent pumping system is described in some depth. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 84A10929
AIAA PAPER 83-2581 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/401000 |
