Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page viii
... Outer Planet Entry Heating , and II ) Thermal Protection Systems . Chapter I consists of nine papers concerned with further development and understanding of aerothermodynamic environment and heating of outer planet probes . The basic ...
... Outer Planet Entry Heating , and II ) Thermal Protection Systems . Chapter I consists of nine papers concerned with further development and understanding of aerothermodynamic environment and heating of outer planet probes . The basic ...
Page ix
... outer planet en probes and re - entry vehicles . Included are papers related to response of materials to intense radiation environments , heat - shield analysis for outer planet entry probes , and a number of papers on the development ...
... outer planet en probes and re - entry vehicles . Included are papers related to response of materials to intense radiation environments , heat - shield analysis for outer planet entry probes , and a number of papers on the development ...
Page 20
... Entry Probes , " Progress in Astronautics and Aeronautics : Thermophysics of Spacecraft and Outer Planet Entry Probes , Vol . 56 , edited by A. M. Smith , AIAA , New York , 1977 , pp . 333-354 . 11 6Sutton , K. , Jones , J. J. , and ...
... Entry Probes , " Progress in Astronautics and Aeronautics : Thermophysics of Spacecraft and Outer Planet Entry Probes , Vol . 56 , edited by A. M. Smith , AIAA , New York , 1977 , pp . 333-354 . 11 6Sutton , K. , Jones , J. J. , and ...
Contents
Effects of Atmospheric Structure on Radiative Heating | 3 |
Radiative Flux Penetration through a Blown Shock Layer | 22 |
Approximate Inviscid Radiating Flowfield Analysis | 42 |
Copyright | |
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Common terms and phrases
ablation absorption coefficient AIAA AIAA Journal AIAA Paper altitudes analysis angle of attack base blockage body surface boundary layer bow shock calculations carbon phenolic chemical chemical equilibrium computed configuration correlation distribution energy enthalpy entry conditions equilibrium experimental flow flowfield freestream graphite H₂ heat shield Heat Transfer heat-transfer hydrogen hyperboloid inertial entry angle intensity inviscid Jupiter Jupiter entry km/sec laminar laser mass loss mass transfer material mixture model atmospheres MW/m² NASA nominal nondimensional nonequilibrium number density obtained Outer Planet Entry parameters PRECURSOR EFFECT precursor heating precursor region predicted present pressure radiation radiative and convective radiative flux radiative heat flux radiative heating rates recession Reynolds number shock-layer shown in Fig silica solution species spectral spectral flux sphere-cone stagnation point stagnation-point temperature thermal thermochemical thermodynamic tion trajectory turbulent uncertainty variation velocity viscous shock-layer VSL3D wall