Flight Qualified Pulsed Electric Thruster for Satellite Control
Author:
Affiliation:
1. MIT Lincoln Laboratory, Lexington, Mass.
2. Los Alamos Scientific Laboratory, Los Alamos, N. Mex.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.62141
Reference13 articles.
1. Pulsed plasma microthruster propulsion system for synchronous orbit satellite
2. Analysis of solid Teflon pulsed plasma thruster
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4. Performance Study of a Solid Fuel-Pulsed Electric Microthruster
5. Interferometric Density Measurements in the Arc of a Pulsed Plasma Thruster
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