| タイトル | Development and Testing of a Methane/Oxygen Catalytic Microtube Ignition System for Rocket Propulsion |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120018040 |
| 著者（英） | Deans, Matthew |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2012-07-31 |
| 言語 | eng |
| 内容記述 | This study sought to develop a catalytic ignition advanced torch system with a unique catalyst microtube design that could serve as a low energy alternative or redundant system for the ignition of methane and oxygen rockets. Development and testing of iterations of hardware was carried out to create a system that could operate at altitude and produce a torch. A unique design was created that initiated ignition via the catalyst and then propagated into external staged ignition. This system was able to meet the goals of operating across a range of atmospheric and altitude conditions with power inputs on the order of 20 to 30 watts with chamber pressures and mass flow rates typical of comparable ignition systems for a 100 lbf engine. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | E-18451-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/239789 |
