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NASA NTRS · 19770004160

Performance documentation of the engineering model 30-cm diameter thruster

Abstract

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 are presented. Performance data for the nominal fullpower (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 are included). 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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BibTeXRIS

Bechtel, R. T., Rawlin, V. K.. 1976-01-01. Performance documentation of the engineering model 30-cm diameter thruster. https://ntrs.nasa.gov/citations/19770004160

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