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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.
Series
EES Examensarbete / Master Thesis
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-91304OAI: oai:DiVA.org:kth-91304DiVA: diva2:509361
Uppsok
Physics, Chemistry, Mathematics
Supervisors
Examiners
Available from: 2012-03-20 Created: 2012-03-12 Last updated: 2012-03-20Bibliographically approved

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fulltext(4750 kB)398 downloads
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File name FULLTEXT01.pdfFile size 4750 kBChecksum SHA-512
f3824d910a40e079b6213e83dfcce8b68dac84e2f4e5b9b629409211133014d3f4e250c5da45793fbdca82247814fa0f643454aa5358756be9714be860f07db9
Type fulltextMimetype application/pdf

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CiteExportLink to record
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