| タイトル | Fly-away restraint pin mechanism for the Army's PATRIOT missile system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790013207 |
| 著者（英） | Knight, F. W. |
| 著者所属（英） | Martin Marietta Corp. |
| 発行日 | 1977-04-28 |
| 言語 | eng |
| 内容記述 | The development of the longitudinal restraint mechanism for the Army's Patriot missile system is reviewed. The initial design was an ordnance pin puller with a shear plane. Because of reliability problems and a desire to reduce cost, a fly-away restraint mechanism was chosen. After being manually unlocked, the restraint pin disengages the missile during launch by missile motion. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 79N21378 |
| 権利 | No Copyright |
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