Preliminary plume characteristics of an arcjet thruster
Author:
Affiliation:
1. Sverdrup Technology, Inc., BrookPark, OH
2. NASA, Lewis Research Center, Cleveland, OH
3. Stuttgart, Universitaet, Federal Republic of Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2645
Reference24 articles.
1. Performance characterization of a low power hydrazine arcjet
2. An extended life and performance test of a low-power arcjet
3. The effects of arcjet thruster operating condition constrictor geometry on the plasma plume
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