Thermal analysis of a Star Sensor Bracket for a satellite (detailed FE model - ANSYS) Thermal analysis of a Star Sensor Bracket for a satellite (ESATAN model)
Static and transient analyses (temperature distribution, heat flow)
Evaluation of the thermal balance of active and passive components
Design optimisation based on many years of experience and numerical methods
Abstraction and implementation of complex thermal boundary conditions in mathematical models
Tools: ANSYS (FEM), ESATAN-TMS
ANSYS (FEM)
Applied for the complete spectrum of thermal analyses
Realisation of detailed, parametric models
Numerical design optimisation and sensitivity studies
ESATAN-TMS:
Thermal analyses for space projects
Model derivation from CAD-geometry and FEM-models
Direct generation of detailed and reduced geometric and thermal models (GMM und TMM)
Computation of specific parameters required for ESATAN models by detailed FEM simulations