Development of Electric and Chemical Microthrusters
Author:
Affiliation:
1. Department of Aerospace Engineering, KAIST, Daejeon 305-701, Republic of Korea
2. Aerospace Engineering Department, University of Applied Sciences at Wiener Neustadt, 2700 Wiener Neustadt, Austria
Abstract
Publisher
Hindawi Limited
Subject
Aerospace Engineering
Link
http://downloads.hindawi.com/journals/ijae/2011/361215.pdf
Reference4 articles.
1. Liquid-metal-ion source development for space propulsion at ARC
2. Indium Field Emission Electric Propulsion Microthruster Experimental Characterization
3. 2000-Hour Endurance Test of Indium Field Emission Electric Propulsion Microthruster Cluster
4. High current liquid metal ion source using porous tungsten multiemitters
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