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dc.contributor.authorHogstad, Rita Henriksen
dc.contributor.authorWong, Ming Kit
dc.contributor.authorFegri, Erica
dc.contributor.authorSkjelsbæk, Jon
dc.contributor.authorMundal, Thomas
dc.contributor.authorØstrem, Håvar
dc.date.accessioned2019-06-28T13:29:04Z
dc.date.available2019-06-28T13:29:04Z
dc.date.issued2019
dc.identifier.urihttp://hdl.handle.net/11250/2602843
dc.description.abstractA rapidly expanding market for Cubesats encourages companies to explore business opportunities by innovating new solutions for use on small satellites. Cubesat is aimed to be modular and easily accessible for any who want to launch satellites into space. Cubesats larger than 8U has never been launched before, and even though these are still small satellites, they may require a more reliable power source than normally accessible on a conventional Cubesat. En-gineering a solution for power collection and transfer has for larger satellites traditionally been tailored for each different satellite. Since Cubesat is aiming to standardize components, there may be a demand for a power transfer system for Cubesats larger than 8U when these become the norm. This report discusses a solution to a Solar Array Drive Mechanism for Cubesats as a plug-and-play solution, including power transfer and test bench.nb_NO
dc.language.isoengnb_NO
dc.publisherUniversitetet i Sørøst-Norge, Fakultet for teknologi og maritime fagnb_NO
dc.titleSatLightnb_NO
dc.typeBachelor thesisnb_NO
dc.rights.holder© Forfatternenb_NO
dc.source.pagenumberFlere pag.nb_NO


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