The High Power Electric Propulsion (HiPEP) Ion Thruster

Practical implementation of the proposed Jupiter Icy Moon Orbiter (JIMO) mission, which would require a total delta V of approximately 38 km/s, will require the development of a high power, high specific impulse propulsion system. Initial analyses show that high power gridded ion thrusters could sat...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Foster, John E., Haag, Tom, Patterson, Michael, Williams, George J., Jr, Sovey, James S., Carpenter, Christian, Kamhawi, Hani, Malone, Shane, Elliot, Fred
Format:	Report
Sprache:	eng
Schlagworte:	Spacecraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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