NASA NTRS ยท 19850002823
Characterization of 8-cm engineering model thruster
Abstract
Development of 8 cm ion thruster technology which was conducted in support of the Ion Auxiliary Propulsion System (IAPS) flight contract (Contract NAS3-21055) is discussed. The work included characterization of thruster performance, stability, and control; a study of the effects of cathode aging; environmental qualification testing; and cyclic lifetesting of especially critical thruster components.
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Williamson, W. S.. 1984-03-01. Characterization of 8-cm engineering model thruster. https://ntrs.nasa.gov/citations/19850002823
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