Modeling plasma processes in 1 kW hydrazine arcjet thrusters

Author:

Megli Thomas1,Lu Junqing1,Krier Herman1,Burton Rodney1

Affiliation:

1. Illinois, Univ., Urbana

Publisher

American Institute of Aeronautics and Astronautics

Reference32 articles.

1. 2Tiliakos, N. T., Burton, R. L., and Krier, H, "Energy Transfer at the Anode of a 1 kW Arcjet," AIAAPaper 96-2964,1996.

2. 3Butler,G.W.,Cassady,R.J., andKing,D.Q."Directions for Arcjet Technology Development," AIAAPaper 94-2652,1994.

3. 4Megli, T. W. "A Nonequilibrium Plasmadynamics Model for Nitrogen/Hydrogen Arcjets," Ph.D. Thesis,Department of Mechanical and Industrial Engineering,University of Illinois at Urbana-Champaign,1995.

4. Sutton and Sherman, Engineering Magneto-Hydrodynamics.McGraw-Hill, NewYork, 1965, pp.148-190.

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