| タイトル | Design and structural analysis of Mars Rover RTG |
| 著者（英） | Sankarankandath, Kumar; Schock, Alfred; Hamrick, Thomas; Shirbacheh, Michael |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1992-01-01
1992 |
| 言語 | eng |
| 内容記述 | The Mars Rover and Sample Return mission's radioisotope thermoelectric generator (RTG) is presently subjected to a structural and mass analysis in view of a reference mission scenario, an illustrative Rover design and Martian activities agenda, and RTG power system requirements and environmental constraints. The modular heat-source stack in the Rover RTG can be held together by axial load springs. The RTGs should be mounted on the Rover with a vertical orientation, in order to avoid the buildup of windborne Martian sand on its heat-rejection surfaces. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 93A20770 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/321208 |
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