High Voltage Solar Array Development for Space and Thruster-Plume Plasma Environments
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA
Funder
Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Condensed Matter Physics,Nuclear and High Energy Physics
Link
http://xplorestaging.ieee.org/ielx7/27/9735185/09714204.pdf?arnumber=9714204
Reference20 articles.
1. Electrostatic Discharge Tests of Solar Array Coupons With Different String-to-String Gaps Without RTV Adhesive Grout
2. The worst-case GEO environment and the frequency of arcs;ferguson;Proc 13th Spacecraft Charging Technol Conf,2014
3. Possible Decline in Solar Array Performance Due to Electrostatic Discharges in Orbit
4. Definitive high voltage solar array testing in space and thruster plume plasma environments;goebel;Proc 13th Spacecraft Charging Technol Conf,2014
5. Fundamentals of Electric Propulasion
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