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hypersonicPRJ

This project simulates the Orion capsule descend on Mars.

The descend has been modeled using SPARTA code.

Simulations

The simulated cases are the following:

Case Mesh Description Output
aeroCoeffCase 3D C & O based molecules simulation without reactions CL & CD analysis with respect to Mach, Knundsen and AOA
basicReactiveCase 2D C & O based molecules simulation with reactions Flow study
extendedReactiveCase 2D C, O, N & e- based molecules simlation with reactions Flow study

The results of the simulation are summed up on these slides.

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Politecnico di Milano hypersonic flow course project.

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