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The High Power Electric Propulsion (Hipep) Ion Thruster - Nasa Technical Reports Server (Ntrs) (Creator), and Et Al (Creator), and Foster, John E
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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 satisfy JIMO mission requirements. A NASA GRC-led team is developing a large area, high specific impulse, nominally 25 kW ion thruster to satisfy both the performance and the lifetime requirements for this proposed mission. The ...

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The High Power Electric Propulsion (Hipep) Ion Thruster 2013, Bibliogov

ISBN-13: 9781287265283

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