| タイトル | Systems constraints imposed on spacecraft utilizing long extendable rods with attached tip masses. |
| 著者（英） | Josloff, A. T. |
| 発行日 | 1967-01-01 |
| 言語 | eng |
| 内容記述 | Systems constraints imposed on spacecraft utilizing long flexible rods with attached tip masses, specifically deployment and retraction problems |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 67A23757 |
| 権利 | Copyright |
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