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Sub-micronewton thrust measurements of indium field emission thrustersThe 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.
Document ID
20060028813
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/7113
Authors
Ziemer, J. K.
Date Acquired
August 23, 2013
Publication Date
March 17, 2003
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
electric propulsion field effect thruster FEEP

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