Experimental investigation of steady state high power MPD thrusters-Reference-Cited by-同舟云学术

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Experimental investigation of steady state high power MPD thrusters

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

WEGMANN THOMAS¹,AUWETER-KURTZ MONIKA¹,HABIGER HARALD¹,KURTZ HELMUT¹,SCHRADE HERBERT¹

Affiliation:

1. Stuttgart, Universitaet, Federal Republic of Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3464

Reference26 articles.

1. Optimization of electric propulsion systems considering specific power as function of specific impulse

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1. Spectroscopic diagnosis and simulation analysis of tungsten cathode erosion during the start-up process for a magnetoplasmadynamic thruster;Vacuum;2023-12

2. Temperature measurement and simulation analysis of heaterless hollow cathode during start-up process;Journal of Physics D: Applied Physics;2022-09-28

3. Simplified model for the evaluation of the Magnetic Nozzle effect on the AF-MPDT in low discharge current to mass flow rate ratio regime;2018 Joint Propulsion Conference;2018-07-08

4. Optimization of the AF-MPDT geometry and operating parameters for the low current to mass flow rate ratio regime;2018 Plasmadynamics and Lasers Conference;2018-06-24

5. Thrust Performance and Cathode Temperature Evaluation of MW Class Quasi-Steady MPD Thruster;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

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