Performance of Miniature Microwave Discharge Ion Thruster for Drag-free Control-Reference-Cited by-同舟云学术

Performance of Miniature Microwave Discharge Ion Thruster for Drag-free Control

Published:2012-07-30 Issue: Volume: Page:
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Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Izumi Takehiro,Koizumi Hiroyuki,Yamagiwa Yoshiki,Matsui Makoto,Kuninaka Hitoshi

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. 2D.DiCara,S.Strandmoe,J.A.RomeraPerez,L.Stagnaro,H.Leiter,andR.Killinger, etal."RITMicroPropulsionSystem on LisaPathfinder", InternationalElectricPropulsion Conference,IEPC-2011-325.

2. 3C. Scharrlemann, A. Genovese, R. Schnitzer, N. Buldrini, P. Sattler, M. Tajimar, "In-FEEP Endurance Test for LISA PF", AIAA-2009-5093,45th jointPropulsionConference, Denver, Colorado,2009.

3. Miniature Microwave Discharge Ion Thruster Driven by 1 Watt Microwave Power

4. 5Koizumi, H., and Kuninaka, H. "Ion BeamExtraction and Electron Emission fromtheMiniatureMicrowaveDischargeIon Engine 1", InternationalElectricPropulsion Conference, IEPC-2009-178.

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