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NASA NTRS ยท 19780018229

Ion Propulsion for Spacecraft

Abstract

The theory of the ion-thruster propulsion system is discussed along with the Space Electric Rocket Test 1 and 2. The use of electric propulsion for stationkeeping and attitude control functions of geosynchronous satellites is described, and a comparison of thruster systems is presented.

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BibTeXRIS

Kerslake, W. R.. 1977-01-01. Ion Propulsion for Spacecraft. https://ntrs.nasa.gov/citations/19780018229

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