Development of an 8-cm engineering model thruster system
Author:
Affiliation:
1. Hughes Research Laboratories, Malibu, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1976-1058
Reference10 articles.
1. J. Hyman. Jr. "Development of a 5 5 m Flight-CAalified M e r c u r y Ion T h r u s t e r , ( ' J o u r n a l of Sp a c e c r a f tand Rockets. Vol.10. Aug. 1973, pp.503-509.
2. S. Nakanishi and R. C. Finke, "A 9700-Hour Durability T e s t of a Five C e n t i m e t e r Diame t e r Ion T h r u s t e r , " AIAA P a p e r No. 73- 11 11, AlAA 10th E l e c t r i c P r o p u l s i o n Conference, Oct. 31-Nov. 2, 1973, Stateline, Nevada.
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2. Simplification of power electronics for ion thruster neutralizers;Journal of Spacecraft and Rockets;1984-09
3. Simplified Power Supplies for Ion Thrusters;Journal of Spacecraft and Rockets;1982-09
4. Simplified power supplies for ion thrusters;15th International Electric Propulsion;1981-04-21
5. Modularized Ion Thruster Development for Auxiliary Propulsion;Journal of Spacecraft and Rockets;1978-05
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