High Performance Power Module for Hall Effect Thrusters-Reference-Cited by-同舟云学术

High Performance Power Module for Hall Effect Thrusters

Published:2002-07-07 Issue: Volume: Page:
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Container-title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Pinero Luis,Bowers Glen

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. Oleson, S. R. "Advanced Hall Electric Propulsion for Future In-Space Transportation", 3rd International Conference on Spacecraft Propulsion, Cannes, France, October, 2000.

2. Oleson, S. R. "Mission Advantages of Constant Power, Variable Isp Electrostatic Thrusters," AIAA-2000-3413, 36thJoint Propulsion Conference, Huntsville, Alabama, July, 2000.

3. Oleson, S. R. "Advanced Electric Propulsion for RLV Launched Geosynchronous Spacecraft," IEPC 99-185, 26thInternational Electric Propulsion Conference, Kitakyushu, Japan, October, 1999.

4. Oleson, S. R. "Advanced Electric Propulsion For Space Solar Power Satellites," AIAA-99-2872, 35thJoint Propulsion Conference, June, 1999.

5. Advanced Propulsion for Geostationary Orbit Insertion and North-South Station Keeping

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