Discharge reliability in ablative pulsed plasma thrusters
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
1. Pulsed plasma thruster;Burton;J. Propuls. Power,1998
2. Correction thruster development based on high-current surface discharge in vacuum;Silnikov;Acta Astronaut.,2014
3. Results of the qualification test campaign of a Pulsed Plasma Thruster for Cubesat Propulsion (PPTCUP);Ciaralli;Acta Astronaut.,2016
4. Pulsed plasma thruster performance for miniaturised electrode configurations and low energy operation;Pottinger;Acta Astronaut.,2011
5. Characteristics of plasma properties in an ablative pulsed plasma thruster;Schönherr;Phys. Plasmas,2013
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