| タイトル | A clamp mechanism for deployable three-ton payloads |
| 著者（英） | Ral, H.; Birner, R. |
| 著者所属（英） | Messerschmitt-Boelkow-Blohm G.m.b.H. |
| 発行日 | 1981-05-01 |
| 言語 | eng |
| 内容記述 | The requirements, capabilities, and unique design features of the instrument payload subsystem payload clamp assembly (PCA) are presented. The PCA is designed to have the flexibility to accommodate a wide payload range varying from 0.5 m to 3 m in diameter and from 500 kg to 3000 kg mass. This is achieved by modular clamp design in connection with replaceable struts. The design features include clamping of payload in a statically determined way and actuation of clamp latches by means of single linear actuator via ropes. The vibration and TV environmental conditions for the mechanism are extremely severe. A structural and prototype model was built. Test results of the operating characteristic are presented. In addition, problems of tribology are highlighted. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 81N22413 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/531023 |
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