High-power hydrogen arcjet performance-Reference-Cited by-同舟云学术

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High-power hydrogen arcjet performance

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:27th Joint Propulsion Conference
language:
Short-container-title:

Author:

HAAG THOMAS¹,CURRAN FRANCIS¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-2226

Reference27 articles.

1. Characteristicsofa 30KWThermalArcjetEngine for SpacePropulsion." AIAAPaper 86-1508, June 1986. 4. Curran,F.M., and Haag, T.W. "An ExtendedLife

2. andPerformanceTestofaLow-PowerArcjet," AIAAPaper 88-3106,July 1988 5 Haag, T.W., and Curran, F.M. "ArcjetStarting

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Review of High-Power Electrostatic and Electrothermal Electric Propulsion;Journal of Propulsion and Power;2022-11

2. Numerical simulation of hydrogen arcjet thruster with coupled sheath model;Plasma Science and Technology;2022-01-17

3. Thrust Stand Characterization of the NASA NEXT Thruster;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

4. Internal nozzle parameters of a subsonic-anode-attachment medium-power hydrogen arcjet;30th Joint Propulsion Conference and Exhibit;1994-06-27

5. Enhancing U.S. Competitiveness: The NASA Electric PropuIsion Program;30th Joint Propulsion Conference and Exhibit;1994-06-27

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