| タイトル | Tethered subsatellite study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760019165 |
| 著者（英） | Rheinfurth, M. H.; Baker, W. P.; Johnston, K. D.; Dunkin, J. A.; Galaboff, Z. J.; Kissel, R. R.; Siebel, M. P. L. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1976-03-01 |
| 言語 | eng |
| 内容記述 | The results are presented of studies performed relating to the feasibility of deploying a subsatellite from the shuttle by means of a tether. The dynamics, the control laws, the aerodynamics, the heating, and some communication considerations of the tethered subsatellite system are considered. Nothing was found that prohibits the use of a subsatellite joined to the shuttle by a long (100 km) tether. More detailed studies directed at specific applications are recommended. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 76N26253
NASA-TM-X-73314 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/185484 |
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