Thrust and beam profile measurements of indium field effect thrusters
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Engineering topics
Publications and source records attributed to Ziemer, J. K..
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The performance of three indium field emission thrusters (In-FETs) developed by the Austrian Research Center Seibersdorf (ARCS) have been measured up to 200 muN, 2 mA, and 20 W using a submicronewton resolution thrust stand.
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A review of Laser Albation Microthruster (LAmuT) technology along with recent experimental results are presented.
An experimentally verified performance scaling model for gas-fed pulsed plasma thrusters (GFPPTs) is used as part of a mission study for refuelable satellites.
This paper describes the development and testing of a microthrust stand in the Advanced Propulsion Technology Laboratory at NASA/JPL.