Injector design and test for a high power electrodeless plasma thruster
The HPEP (High Performance Electric Propulsion) thruster is expected to be the outcomecof an innovative project initiated by the Swedish Space Corporation. It combines the concept of a 10 kW electrodeless plasma thruster designed by the Elwing Company and the ADN based monopropellant LMP-103S develo...
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| Format: | Others |
| Language: | English |
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KTH, Rymd- och plasmafysik
2011
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-91765 |