Items related to 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 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 design philosophy and development status as well as a thruster performance assessment are presented.
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- PublisherBibliogov
- Publication date2013
- ISBN 10 1287265286
- ISBN 13 9781287265283
- BindingPaperback
- Number of pages24
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