Print Email Facebook Twitter Thermal Modelling & Analysis of the Deployable Space Telescope Title Thermal Modelling & Analysis of the Deployable Space Telescope Author van Wees, Tim (TU Delft Aerospace Engineering) Contributor Kuiper, J.M. (mentor) Zandbergen, B.T.C. (graduation committee) Naeije, M.C. (graduation committee) Degree granting institution Delft University of Technology Programme Aerospace Engineering Date 2019-04-30 Abstract The Deployable Space Telescope (DST) project aims at producing a competitive telescope by using segmented deployable light weighted optics which reduces launch volume and mass, and thus launch costs. Due to the criticality of heat management to the performance of the telescope, a thermal model had to be built in order to determine the expected temperatures throughout the telescope in orbit. Further, the premature baffle design required a supportive thermal analysis such that its critical parameters could be determined. Subject ThermalThermal analysisThermal managementThermal controlSpace telescopeESATAN TMS To reference this document use: http://resolver.tudelft.nl/uuid:f698fca7-205b-487d-b521-83d7f85e6fef Part of collection Student theses Document type master thesis Rights © 2019 Tim van Wees Files PDF MSc_Thesis_TTD_van_Wees.pdf 18.03 MB Close viewer /islandora/object/uuid:f698fca7-205b-487d-b521-83d7f85e6fef/datastream/OBJ/view