| タイトル | Electronic delay ignition module for single bridgewire Apollo standard initiator |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760012256 |
| 著者（英） | Ward, R. D. |
| 著者所属（英） | Vought Corp. |
| 発行日 | 1975-01-01 |
| 言語 | eng |
| 内容記述 | An engineering model and a qualification model of the EDIM were constructed and tested to Scout flight qualification criteria. The qualification model incorporated design improvements resulting from the engineering model tests. Compatibility with single bridgewire Apollo standard initiator (SBASI) was proven by test firing forty-five (45) SBASI's with worst case voltage and temperature conditions. The EDIM was successfully qualified for Scout flight application with no failures during testing of the qualification unit. Included is a method of implementing the EDIM into Scout vehicle hardware and the ground support equipment necessary to check out the system. |
| NASA分類 | ELECTRONICS AND ELECTRICAL ENGINEERING |
| レポートNO | 76N19344
NASA-CR-144898 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186714 |
