| タイトル | Dual shear plate power processor packaging design |
| 著者（英） | Franzon, A. O.; Fredrickson, C. D.; Ross, R. G. |
| 発行日 | 1975-03-01 |
| 言語 | eng |
| 内容記述 | The use of solar electric propulsion (SEP) for spacecraft primary propulsion imposes an extreme range of operational and environmental design requirements associated with the diversity of missions for which solar electric primary propulsion is advantageous. One SEP element which is particularly sensitive to these environmental extremes is the power processor unit (PPU) which powers and controls the electric ion thruster. An improved power processor thermal-mechanical packaging approach, referred to as dual shear plate packaging, has been designed to accommodate these different requirements with minimum change to the power processor design. Details of this packaging design are presented together with test results obtained from thermal-vacuum and structural-vibration tests conducted with prototype hardware. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75A26572
AIAA PAPER 75-382 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/448605 |
