| タイトル | Characteristics of primary electric propulsion systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790022119 |
| 著者（英） | Byers, D. C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | The use of advanced electric propulsion systems is expected to provide cost and performance benefits for future energetic space missions. A methodology to predict the characteristics of advanced electric propulsion systems was developed and programmed for computer calculations to allow evaluation of a broad set of technology and mission assumptions. The impact on overall thrust system characteristics was assessed for variations of propellant type, total accelerating voltage, thruster area, specific impulse, and power system approach. The data may be used both to provide direction to technology emphasis and allow for preliminary estimates of electric propulsion system properties for a wide variety of applications. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 79N30290
NASA-TM-79255
E-166 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/174782 |
