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1 Geometry 1 Mesh 1 Simulation setup 2 ResultsAbout this project
This project is a preliminary case study to understand the effects of varying extreme temperatures in space on the Cubesat. The Satellite is approximated to be a cuboid shell with dimensions of 10 X 10 X 30 cm3. The boundary conditions are set such that one phase is always facing the sun and is subject to extreme temperatures while the other end is always fixed.
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by Ali_ArafatAli_Arafat
Project History
Blaze created this project