| タイトル | Development of a Enhanced Thermal Barrier for RSRM Nozzle Joints |
| 著者（英） | McCool, A.; Bauer, P. H. |
| 著者所属（英） | Thiokol Propulsion |
| 発行日 | 2000-01-01 |
| 言語 | eng |
| 内容記述 | A carbon fiber rope is being considered as replacement for the RTV thermal barrier that is currently used to protect o-rings in RSRM nozzle joints, Performance requirements include its ability to cool propellant gases filter slag and particulates, and conform to various joint assembly conditions as well as dynamic flight motion. Testing has shown its superior heat resistance, even in oxidative and corrosive environments. Testing has also demonstrated excellent performance of this system in sub-scale motors. Cold flow testing, has demonstrated its ability to conform to motor dynamics. Manufacture and assembly testing have demonstrated the ease of gland machining as well as assembly in a full-scale nozzle. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/340179 |
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