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Design and analysis of mission and system requirements for 'NetSat' mission with respect to structural and thermal limitations
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
2019 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

In the scope of this master thesis work, the proposed design for NetSat was analyzed for mission and system requirements with respect to structural and thermal limitations. Different load case scenarios for structural and thermal analysis were considered during the process which have been discussed. Based on results, the design is qualified and expected to satisfy all mission and system requirements with regards to structural and thermal limitations.

Place, publisher, year, edition, pages
2019. , p. 64
Keywords [en]
Structural analysis, thermal analysis, 3U cubesat, NetSat
National Category
Other Engineering and Technologies not elsewhere specified
Identifiers
URN: urn:nbn:se:ltu:diva-76336OAI: oai:DiVA.org:ltu-76336DiVA, id: diva2:1359613
External cooperation
Zentrum Für Telematik e.V (ZfT, Würzburg, Germany)
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level (120 credits)
Presentation
2019-09-11, Kiruna, 15:00 (English)
Supervisors
Examiners
Available from: 2019-10-10 Created: 2019-10-09 Last updated: 2019-10-10Bibliographically approved

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CiteExportLink to record
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Citation style
  • apa
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  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
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  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf