| タイトル | The Cassini Main Engine Assembly Cover Mechanism |
| 著者（英） | Sevilla, Donald R. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1997-05-01 |
| 言語 | eng |
| 内容記述 | This paper describes a micrometeroid protection system for the main engines of the Cassini spacecraft. The engine Cover Assembly is a deployable/restowable half sphere of multilayer insulation mounted to an articulatable frame over 2 meters (7 feet) in diameter. The Cover folds into a compact wedge only 25 cm (10 inches) at its maximum thickness. The micrometeroid environment and typical protection methods are described as well as the design details and development problems of the Cover Mechanism Assembly. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | 97N22556 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/541661 |
