| タイトル | Mission and System Advantages of Iodine Hall Thrusters |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140012585 |
| 著者（英） | Kamhawi, Hani; Pote, Bruce; Szabo, James; Dankanich, John W.; Oleson, Steve |
| 発行日 | 2014-07-28 |
| 言語 | eng |
| 内容記述 | The exploration of alternative propellants for Hall thrusters continues to be of interest to the community. Investments have been made and continue for the maturation of iodine based Hall thrusters. Iodine testing has shown comparable performance to xenon. However, iodine has a higher storage density and resulting higher V capability for volume constrained systems. Iodine's vapor pressure is low enough to permit low-pressure storage, but high enough to minimize potential adverse spacecraft-thruster interactions. The low vapor pressure also means that iodine does not condense inside the thruster at ordinary operating temperatures. Iodine is safe, it stores at sub-atmospheric pressure, and can be stored unregulated for years on end; whether on the ground or on orbit. Iodine fills a niche for both low power (<1kW) and high power (>10kW) electric propulsion regimes. A range of missions have been evaluated for direct comparison of Iodine and Xenon options. The results show advantages of iodine Hall systems for both small and microsatellite application and for very large exploration class missions. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | M14-3883 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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