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Engineering
Solutions
International
Limited
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ESIL
has a number of years experience in Space engineering with
current and past projects including;
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Hypersonic Flow and Thermal
Protection System (TPS).
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Thermal Protection System (TPS)
Behaviour at Hypersonic Planetary Re-Entry.
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Study of Ablative Materials
Properties.
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Coupling Ablation Code with
CFD-Code.
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Implementation of Subroutines
in the Codes.
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Implementation of the Data in
Trajectory Code and CFD Code.
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Simulation of Spacecraft
Re-Entry at Hypersonic Velocity.
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Coupling the CFD Results with
Radiation Code for Heat Flux Prediction
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Fluid-Structure Interaction
Modelling
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Multiphysics Code Coupling
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Catalysis Modelling
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