A Critical Review of Thrust Models for Applied-Field Magnetoplasmadynamic Thrusters
Author:
Affiliation:
1. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4723
Reference76 articles.
1. Characteristics and local analysis of MPD THRUSTER operation
2. Advanced scaling model for simplified thrust and power scaling of an applied-field magnetoplasmadynamic thruster
3. 6L. K. Rudolph. The MPD Thruster Onset Current Performance Limitation. PhD thesis,Princeton University, Sept. 1980.
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