Pulsed Plasma Thruster Performance for Microspacecraft Propulsion-Reference-Cited by-同舟云学术

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Pulsed Plasma Thruster Performance for Microspacecraft Propulsion

Published:2000-01-01 Issue: Volume: Page:337-352
ISSN:
Container-title:Micropropulsion for Small Spacecraft
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Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600866586.0337.0352

Reference41 articles.

1. Pulsed Plasma Thruster

2. 3Sedwick,R. J., Kong,E. M. C.,and Miller,D. W. "Exploiting OrbitalDynamicsand MicropropulsionforApertureSynthesisUsingDistributedSatelliteSystems:Applications toTechSat 21,"AIAAPaperNo.98-5289, 1998.

3. 5Bushman,S. S. "Investigationsof a Coaxial Pulsed Plasma Thruster," M.S. Thesis, Rept.No. UILU 99-0509,Dept. of Aeronauticaland AstronauticalEngineering,Univ.of Illinois,Urbana,IL,1999.

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2. Analysis of Fiber-Fed Pulsed Plasma Thruster Performance;Journal of Propulsion and Power;2021-01

3. Thrusters: Pulsed Plasmas;Encyclopedia of Plasma Technology;2016-12-12

4. A new stage in the development of ablative pulsed plasma thrusters at the RIAME;Solar System Research;2012-12

5. Performance Evaluation of Powdered Propellant Pulsed Plasma Thruster;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

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