| タイトル | Rocket Launch-Induced Vibration and Ignition Overpressure Response |
| 本文（外部サイト） | http://hdl.handle.net/2060/20010038008 |
| 著者（英） | Margashayam, Ravi N.; Nayfeh, Jamal F.; Thompson, Karen; Caimi, Raoul E. |
| 著者所属（英） | NASA Kennedy Space Center |
| 発行日 | 2001-01-01 |
| 言語 | eng |
| 内容記述 | Rocket-induced vibration and ignition overpressure response environments are predicted in the low-frequency (5 to 200 hertz) range. The predictions are necessary to evaluate their impact on critical components, structures, and facilities in the immediate vicinity of the rocket launch pad. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/226297 |
