| タイトル | TOPS attitude propulsion subsystem technology |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720003198 |
| 著者（英） | Moynihan, P. I. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1971-10-01 |
| 言語 | eng |
| 内容記述 | The thermoelectric outer-planet spacecraft (TOPS) attitude propulsion subsystem effort is summarized. It includes the tradeoff rationale that went into the selection of anhydrous hydrazine as the propellant, and a brief description of three types of 0.445-N (100-mlbf) thrusters that were purchased for in-house evaluation. A discussion is also included of the 0.2224-N (50-mlbf)-developed thrusters and their integration with a portable, completely enclosed, propulsion module that was designed and developed to support the TOPS single-axis attitude control tests in the celestarium. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 72N10847 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/571033 |
