Print Email Facebook Twitter Deployable Space Telescope Title Deployable Space Telescope: Redesign of the secondary mirror support structure Author Akkerhuis, Ilja (TU Delft Aerospace Engineering; TU Delft Space Engineering) Contributor Bouwmeester, J. (mentor) Gill, E.K.A. (graduation committee) Kuiper, J.M. (mentor) de Vet, S.J. (mentor) Degree granting institution Delft University of Technology Programme Aerospace Engineering Project Deployable Space Telescope Date 2020-10-06 Abstract The need for higher spatio-temporal resolution Earth observation increases rapidly. To fill this need, the Deployable Space Telescope (DST) project aims to make a light-weight, low-volume deployable telescope. In doing so, the achievable ground resolution is high while the cost per telescope stays low. This allows for the DST to be used in constellations, thus effectively achieving a high spatio-temporal resolution. One of the issues of this design are the relative translation and rotation of the secondary mirror due to temperature fluctuations. This thesis work focused on first finding these movements by identifying the temperature variations of the secondary mirror support structure using ESATAN TMS simulations, and subsequently designing a system to keep these movements within the allowed budgets. The end-result is a novel design in which all displacements are measured by means of 4 Displacement Measuring Interferometers and corrected by means of 4 linear piezo actuators. Subject DeployableSpaceTelescopePiezoelectric actuatorsdisplacement measuring interferometerStabilitysatellite To reference this document use: http://resolver.tudelft.nl/uuid:2c9a8058-85fe-4273-97b7-ec4bc3f61805 Part of collection Student theses Document type master thesis Rights © 2020 Ilja Akkerhuis Files PDF Thesis_Ilja_Akkerhuis_23_ ... 9_2020.pdf 12.81 MB Close viewer /islandora/object/uuid:2c9a8058-85fe-4273-97b7-ec4bc3f61805/datastream/OBJ/view