| タイトル | Project Morpheus Main Engine Development and Preliminary Flight Testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/20110014012 |
| 著者（英） | Morehead, Robert L. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2011-07-30 |
| 言語 | eng |
| 内容記述 | A LOX/Methane rocket engine was developed for a prototype terrestrial lander and then used to fly the lander at Johnson Space Center. The development path of this engine is outlined, including unique items such as variable acoustic damping and variable film cooling. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | JSC-CN-24268 |
| 権利 | No Copyright |
