W. R. Kerslake
Abstract
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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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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.
Key concepts: Spacecraft propulsion, Ion thruster, Geosynchronous orbit, Propulsion, Electrically powered spacecraft propulsion, Spacecraft, Aerospace engineering, Laser propulsion