Development Toward a Spaceflight Capable VASIMR® Engine and SEP Applications
Author:
Affiliation:
1. Ad Astra Rocket Company
2. University of Houston
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-4173
Reference20 articles.
1. 1Longmier, B., Cassady, L., Ballenger, M., Carter,M.,Chang-Díaz, F.,Glover, T., Ilin, A., McCaskill, G., Olsen, C., Squire, J., Bering, E., VX-200 Magnetoplasma Thruster PerformanceResultsExceedingFifty-Percent Thruster Efficiency, AIAA Journal of Propulsion andPower,Vol.27, No.4,2011.
2. Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
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1. Steady-state Testing at 100 kW in the VASIMR® VX-200SS Project;AIAA Propulsion and Energy 2019 Forum;2019-08-16
2. Run-time Accumulation Testing of the 100 kW VASIMR® VX-200SS Device;2018 Joint Propulsion Conference;2018-07-08
3. Thrusters: Current-Free Plasma;Encyclopedia of Plasma Technology;2016-12-12
4. Advances in Duration Testing of the VASIMR® VX-200SS™ System;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22
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