| タイトル | Shuttle subscale ablative nozzle tests |
| 著者（英） | Powers, L. B.; Bailey, R. L. |
| 著者所属（英） | NASA Marshall Space Flight Center|Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1980-06-01 |
| 言語 | eng |
| 内容記述 | Recent subscale nozzle tests have identified new and promising carbon phenolic nozzle ablatives which utilize staple rayon, PAN, and pitch based carbon cloth. A 4-inch throat diameter submerged test nozzle designed for the 48-inch Jet Propulsion Laboratory char motor was used to evaluate five different designs incorporating 20 candidate ablatives. Test results indicate that several pitch and PAN-based carbon phenolic ablatives can provide erosion and char performance equivalent or superior to the present continuous rayon-based SRM ablative. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 80A41179
AIAA PAPER 80-1102 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/421235 |
