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Modelling of plasma thruster plumes for spacecraft-plume impingement analysis
KTH, School of Electrical Engineering (EES), Space and Plasma Physics.
2010 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Place, publisher, year, edition, pages
2010. , 64 p.
EES Examensarbete / Master Thesis
National Category
Aerospace Engineering
URN: urn:nbn:se:kth:diva-91304OAI: diva2:509361
Physics, Chemistry, Mathematics
Available from: 2012-03-20 Created: 2012-03-12 Last updated: 2012-03-20Bibliographically approved

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fulltext(4750 kB)345 downloads
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