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Linking of Liquid Bipropellant Rocket Engine Design Methodology with Launch Vehicle Optimization
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering.
2017 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Place, publisher, year, edition, pages
2017.
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:ltu:diva-66801OAI: oai:DiVA.org:ltu-66801DiVA: diva2:1160882
External cooperation
DLR e.V., Institute of Space Propulsion, Lampoldshausen
Educational program
Space Engineering, master's level (120 credits)
Examiners
Available from: 2017-11-29 Created: 2017-11-28 Last updated: 2017-11-30Bibliographically approved

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CiteExportLink to record
Permanent link

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Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
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