The ablation and ionization characteristics of a rectangular pulsed plasma thruster with hydroxy-terminated polybutadiene propellant
Author:
Affiliation:
1. Beijing Institute of Technology, Beijing 100081, China
Funder
Foundation for Innovative Research Groups of the National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0002936
Reference28 articles.
1. Pulsed Plasma Thruster
2. Plasma acceleration processes in an ablative pulsed plasma thruster
3. Characteristics of plasma properties in an ablative pulsed plasma thruster
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1. Development and Characterization of an Ion Source to Simulate Low Earth Orbit Plasma Environment in a Vacuum Chamber;AIAA SCITECH 2024 Forum;2024-01-04
2. A predictive model for macro-performances applied to laser-assisted pulsed plasma thrusters;Physics of Plasmas;2022-01
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