| タイトル | Hydrazine Gas Generator Program |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750015608 |
| 著者（英） | Kusak, L.; Marcy, R. D. |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1975-03-01 |
| 言語 | eng |
| 内容記述 | The design and fabrication of a flight gas generator for the space shuttle were investigated. Critical performance parameters and stability criteria were evaluated as well as a scaling laws that could be applied in designing the flight gas generator. A test program to provide the necessary design information was included. A structural design, including thermal and stress analysis, and two gas generators were fabricated based on the results. Conclusions are presented. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75N23680
NASA-CR-141795
R-9690 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/190036 |
