Non-equilibrium shock-layer computation for Saturn probes

Statistics – Computation

Scientific paper

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Atmospheric Entry, Saturn (Planet), Shock Layers, Space Probes, Atmospheric Models, Flow Distribution, Flux Density, Heat Shielding, Planetary Atmospheres

Scientific paper

An analytical approach is presented for computing the flow fields, energy fluxes, and heat shield requirements for Saturn probes since total simulation of the shock layer is not feasible. The governing mechanisms are examined and uncoupled, and then put together. Experimental and theoretical inputs are synthesized to provide the necessary information for the heat shield computation.

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