| タイトル | Electron bombardment propulsion system characteristics for large space systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770004163 |
| 著者（英） | Rawlin, V. K.; Byers, D. C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1976-01-01 |
| 言語 | eng |
| 内容記述 | The results of an anlaysis of electron bombardment ion propulsion systems for use in the transportation and on-orbit operations of large space systems are presented. Using baseline technology from the ongoing primary propulsion program and other sources, preliminary estimates of the expected characteristics of key system elements such as thrusters and propellant storage systems were performed. Projections of expected thruster performance on argon are presented based on identified constraints which limit the achievable thrust and/or power density of bombardment thrusters. System characteristics are then evaluated as a function of thruster diameter and specific impulse. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 77N11106
NASA-TM-X-73554
E-8992 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/184052 |
