Energy transfer to the anode of a 1 kW arcjet
Author:
Affiliation:
1. Illinois, Univ., Urbana
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2964
Reference20 articles.
1. 1Soulas, G.C,and Myers, R.M. "Mechanisms of Anode Power Deposition in a Low Pressure Free Burning Arc," NASA Contractor Report 194442, 23rd International Electric Propulsion Conference, IEPCPaperNo.93-194,Sept., 1993.
2. Anode power deposition in magnetoplasmadynamic thrusters
3. Langmuir probe measurements of an arcjet exhaust
4. Exit-plane electrostatic probe measurements of a low-power arcjet
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1. Two-Temperature Chemical-Nonequilibrium Modelling of a High-Velocity Argon Plasma Flow in a Low-Power Arcjet Thruster;Plasma Chemistry and Plasma Processing;2013-10-25
2. Collisionless cathode sheath models to predict power distribution in 1 kW hydrazine arcjets;33rd Joint Propulsion Conference and Exhibit;1997-07-06
3. Modeling plasma processes in 1 kW hydrazine arcjet thrusters;32nd Joint Propulsion Conference and Exhibit;1996-07-01
4. Overview of arcjet thruster research at the University of Illinois;32nd Joint Propulsion Conference and Exhibit;1996-07-01
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