Mission advantages of constant power, variable Isp electrostatic thrusters
Author:
Affiliation:
1. NASA, Glenn Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3413
Reference19 articles.
1. Advanced propulsion for geostationary orbit insertion and north-south station keeping
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