Modulär Mekanikstruktur för Nanosatelliter

The objective of this thesis was to present a design proposal on a modular mechanicalstructure for a nanosatellite. The size of the structure should follow the CubeSatstandards. This standard divides satellites in units (U), where 1U is equivalent to acube where sides measure 100 mm. 2U corresponds...

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Bibliographic Details
Main Authors: Skarpsvärd, Joakim, Helleblad Nymo, Carl-Oscar
Format: Others
Language:Swedish
Published: Uppsala universitet, Industriell teknik 2015
Subjects:
Online Access:http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-256462