| タイトル | Small spacecraft power and thermal subsystems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950018008 |
| 著者（英） | Lambeck, R.; Slifer, L., Jr.; Eakman, D.; Mackowski, M. |
| 著者所属（英） | McDonnell-Douglas Aerospace |
| 発行日 | 1994-12-01 |
| 言語 | eng |
| 内容記述 | This white paper provides a general guide to the conceptual design of satellite power and thermal control subsystems with special emphasis on the unique design aspects associated with small satellites. The operating principles of these technologies are explained and performance characteristics of current and projected components are provided. A tutorial is presented on the design process for both power and thermal subsystems, with emphasis on unique issues relevant to small satellites. The ability of existing technology to meet future performance requirements is discussed. Conclusions and observations are presented that stress cost-effective, high-performance design solutions. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 95N24428
NASA-CR-195029
NAS 1.26:195029 |
| 権利 | No Copyright |
