NASA NTRS · 19770032249
Performance documentation of the Engineering Model 30 cm diameter Thruster
Abstract
Presented are the results of extensive testing of two 30-cm ion thrusters which are virtually identical to the 900 series Engineering Model Thruster in an ongoing 15,000-hour life test. Included are performance data for the nominal full-power (2650 W) operating point; performance sensitivities to discharge voltage, discharge losses, accelerator voltage, and magnetic baffle current; and several power throttling techniques (maximum Isp, maximum thrust/power ratio, and two cases in between). Criteria for throttling are specified in terms of the screen power supply envelope, thruster operating limits, and control stability. In addition, reduced requirements for successful high voltage recycles are presented.
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Bechtel, R. T., Rawlin, V. K.. 1976-11-01. Performance documentation of the Engineering Model 30 cm diameter Thruster. https://ntrs.nasa.gov/citations/19770032249
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