The Radiative Gas Dynamics of a Descent Space Capsule under Conditions of Orbital and Superorbital Entry into the Earth’s Atmosphereстатья
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Дата последнего поиска статьи во внешних источниках: 30 января 2024 г.
Аннотация:The radiative aerothermodynamics of a large-scale segmental-conical spacecraft (SCSC) entering the dense layers of the Earth’s atmosphere at orbital and superorbital velocities is studied. The flow fields of a chemically nonequilibrium compressible viscous and heat-conducting gas near the descent space capsule are numerically calculated in a wide range of flight velocities and altitudes. Regularities in the formation of densities of convective and radiative fluxes on a streamlined surface are discussed.