High Thrust-to-Power Parallel-Rail Pulsed Plasma Thruster Design-Reference-Cited by-同舟云学术

High Thrust-to-Power Parallel-Rail Pulsed Plasma Thruster Design

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:

Kamhawi Hani,Pencil Eric

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Myers, R. "Electromagnetic Propulsion for Spacecraft," AIAA 93-1086, Aerospace Design Conference, Irvine CA, February 1993.

2. Solid-propellant pulsed plasma microthruster studies.

3. Pulsed plasma microthruster propulsion system for synchronous orbit satellite

4. Pencil, E.J., Kamhawi, H., Arrington, L.A., and Warren, W.B. "Evaluation of Alternate Propellants for Pulsed Plasma Thrusters," IEPC 01-147, 27thIEPC, October, 2001.

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