Survey of auxiliary-propulsion systems for communications satellites
Author:
Affiliation:
1. California Institute of Technology, Jet Propulsion Laboratory, Pasadena, Calif.
2. TRW Systems Group, Redondo Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1972-515
Reference66 articles.
1. Prototypes of the LES-6 thruster designed in 1968 were tested extensively in the laboratory. (43) Ground testing was performed at 1 to 4 pps. On several tests the thruster achieved more than 8 million discharges without failure of the capacitor or discharge initiator. lntermittency of discharge. to occur is common with the flight thruster after 1 to 2 million discharges. An intermittent thruster does not draw power, and thus the capacitor can be discharged later. However, when the intermittency becomes more frequent the thruster may never recover. During tests of the LES-6 pulsed plasma thruster at Lincoln Laboratories, one thruster became intermittent after 1 million pulses and did no.t recover. (48)
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1. Performance Trends in Spacecraft Auxiliary Propulsion Systems;Journal of Spacecraft and Rockets;1980-09
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