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1. Finite Element Analysis of Stresses in the MIST CubeSat due to Dynamic Loads During Launch
Master-uppsats, KTH/LättkonstruktionerSammanfattning : A finite element model of the CubeSat MIST was created, in order to assess the stresses that occur in the satellite in response to loads during its launch. Due to size limits of thesoftware used, simplifications had to be made to the geometry of the model. LÄS MER
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