Cathode Sheath Voltage Models for Hydrazine Arcjets

Author:

Lu Junqing1,Krier Herman1,Burton Rodney L.1,Goodfellow Keith D.2

Affiliation:

1. University of Illinois at Urbana – Champaign, Urbana, Illinois 61801

2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Cited by 9 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. Numerical simulation of hydrogen arcjet thruster with coupled sheath model;Plasma Science and Technology;2022-01-17

2. Advanced Validation of Nonequilibrium Plasma Flow Simulation for Arc-Heated Wind Tunnels;Journal of Thermophysics and Heat Transfer;2014-01

3. Thermochemical nonequilibrium modeling of a low-power argon arcjet wind tunnel;Journal of Applied Physics;2013-02-07

4. Improvement of Potential Drop Predictions for Plasma Wind Tunnels by Cathode Sheath;Journal of Thermophysics and Heat Transfer;2012-07

5. Nonequilibrium Plasma Flow Properties in Arc-Heated Wind Tunnels;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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