| タイトル | Design, testing and evaluation of latching end effector |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950020841 |
| 著者（英） | Walker, B.; Vandersluis, R. |
| 著者所属（英） | Spar Aerospace Ltd. |
| 発行日 | 1995-05-01 |
| 言語 | eng |
| 内容記述 | The Latching End Effector (LEE) forms part of the Space Station Remote Manipulator System (SSRMS) for which Spar Aerospace Ltd, Space Systems Division is the prime contractor. The design, testing and performance evaluation of the Latching End Effector mechanisms is the subject of this paper focusing on: (1) ambient, thermal and vibration testing; (2) snare/rigidize performance testing and interaction during payload acquisition; and (3) latch/umbilical test results and performance. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 95N27261 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/107309 |
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