NASA NTRS · 20160004243
Multi-Thruster Propulsion Apparatus
Abstract
An electric propulsion machine includes an ion thruster having a discharge chamber housing a large surface area anode. The ion thruster includes flat annular ion optics with a small span to gap ratio. Optionally, at least a second thruster may be disposed radially offset from the ion thruster.
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Patterson, Michael J.. 2016-03-29. Multi-Thruster Propulsion Apparatus. https://ntrs.nasa.gov/citations/20160004243
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