| タイトル | The hard start phenomena in hypergolic engines. Volume 5: RCS engine deformation and destruct tests |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750004953 |
| 著者（英） | Miron, Y.; Perlee, H. E. |
| 著者所属（英） | Bureau of Mines |
| 発行日 | 1974-03-22 |
| 言語 | eng |
| 内容記述 | Tests were conducted to determine the causes of Apollo Reaction Control (RCS) engine failures. Stainless steel engines constructed for use in the destructive tests are described. The tests conducted during the three phase investigation are discussed. It was determined that the explosive reaction that destroys the RCS engines occurs at the time of engine ignition and is apparently due to either the detonation of the heterogeneous constituents of the rocket engine, consisting primarily of unreacted propellant droplets and vapors, and/or the detonation of explosive materials accumulated on the engine walls from previous pulses. Photographs of the effects of explosions on the simulated RCS engines are provided. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75N13025
NASA-CR-140359
BM-IR-1646-VOL-5 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/191913 |
