Characteristics of a non-volatile liquid propellant in liquid-fed ablative pulsed plasma thrusters
Author:
Affiliation:
1. Komurasaki-Koizumi Laboratory, Department of Aeronautics and Astronautics, The University of Tokyo, 113-8656 Tokyo, Japan
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4975349
Reference40 articles.
1. Pulsed Plasma Thruster
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5. Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster
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