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NASA NTRS · 19680009351

Experimental performance of a low-thrust, divergent-flow, contact-ionization electrostatic thrustor

Abstract

Electrostatic ion thrustor employing cesium on tungsten contact ionization for satellite attitude control and stationkeeping missions

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BibTeXRIS

Lathem, W. C., Staggs, J. F.. 1966-01-01. Experimental performance of a low-thrust, divergent-flow, contact-ionization electrostatic thrustor. https://ntrs.nasa.gov/citations/19680009351

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