Design and experimental results of a laser-ignited solid-propellant-fed magnetoplasmadynamic thruster
Author:
Affiliation:
1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Publisher
AIP Publishing
Subject
Instrumentation
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0006603
Reference23 articles.
1. Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters
2. Analytical investigation of anode heat flux in a magnetoplasmadynamic thruster
3. Numerical Investigation of Plasma Behavior and Anode Sheath in a Magnetoplasmadynamic Thruster
4. Modeling of plasma processes in the slowly diverging magnetic fields at the exit of an applied-field magnetoplasmadynamic thruster
5. A phenomenological performance model for applied-field MPD thrusters
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