| タイトル | System level mechanical testing of the Clementine spacecraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950007674 |
| 著者（英） | Hauser, Joseph; Raynor, William; Lynn, Peter; Haughton, James |
| 著者所属（英） | Kinetic Research Corp. |
| 発行日 | 1994-11-01 |
| 言語 | eng |
| 内容記述 | This paper discusses the system level structural testing that was performed to qualify the Clementine Spacecraft for flight. These tests included spin balance, combined acoustic and axial random vibration, lateral random vibration, quasi-static loads, pyrotechnic shock, modal survey and on-orbit jitter simulation. Some innovative aspects of this effort were: the simultaneously combined acoustic and random vibration test; the mass loaded interface modal survey test; and the techniques used to assess how operating on board mechanisms and thrusters affect sensor vision. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 95N14087 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/109897 |
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