Abstract
The thermal analysis is the major engineering work through the entire satellite development process with some crucial stages such as design, test, and ground operations simulation. In the formal design and verification (by test) phases, a general thermal mathematical model (TMM) for the entire satellite is constructed from a non-linear, time-dependent, partial differential equation with combined heat conduction and radiation inside and environmental heating and cooling as boundary conditions. A few representing numerical schemes with constraints used in the satellite thermal analysis as well as an
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