| タイトル | Noncatalytic hydrazine thruster development - 0.050 to 5.0 pounds thrust |
| 著者（英） | Callens, R. A.; Sackheim, R. L.; Kuenzly, J. D.; Murch, C. K. |
| 著者所属（英） | TRW Defense and Space Systems Group|NASA Goddard Space Flight Center |
| 発行日 | 1976-07-01 |
| 言語 | eng |
| 内容記述 | Noncatalytic (thermal-decompositon) hydrazine thrusters can operate in both the pulsing and steady-state modes to meet the propulsive requirements of long-life spacecraft. The thermal decomposition mode yields higher specific impulse than is characteristic of catalytic thrusters at similar thrust levels. This performance gain is the result of higher temperature operation and a lower fraction of ammonia dissociation. Some life limiting factors of catalytic thrusters are eliminated. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 76A42417
AIAA PAPER 76-658 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/442080 |
