| タイトル | Continuing development of the short-pulsed ablative space propulsion system. |
| 著者（英） | Palumbo, D. J.; Guman, W. J. |
| 発行日 | 1972-11-01 |
| 言語 | eng |
| 内容記述 | Major advancements have been made in solid propellant pulsed plasma propulsion technology. A LES-6 microthruster has operated for 8900 hours in orbit. Millipound thrustors have been developed and tested at performance levels of as low as 112 watts/mlb. Efficiencies of up to 50% and specific impulse values up to 5000 sec have been measured. An improved microthrustor has operated at 207 watts/mlb continuously for 1440 hours. Correlations of design and performance data exist to allow thrustors to be built to meet a particular level of performance. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73A13457
AIAA PAPER 72-1154 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/459534 |
