Thermophysics and Heat Transfer Conference 1974
DOI: 10.2514/6.1974-758
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An approximate inviscid radiating flow-field analysis for sphere-cone Venusian entry vehicles

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Cited by 19 publications
(6 citation statements)
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“…)/ (p w T w ) mol/kg. Under a nonequilibrium sublimation environment the vapor is formed with an evaporation coefficient j8 4 …”
Section: Governing Equationsmentioning
confidence: 99%
See 1 more Smart Citation
“…)/ (p w T w ) mol/kg. Under a nonequilibrium sublimation environment the vapor is formed with an evaporation coefficient j8 4 …”
Section: Governing Equationsmentioning
confidence: 99%
“…The convective and radiative heating rates were determined using the methods described by Moss et al 3 and Falanga and Olstad. 4 The phenomenon of conduction, pyrolysis, ablation of the heat shield, and resulting temperature rise within the heat shield were calculated using a material response code named charring materials ablation (CM A). 5 Accuracy of the CM A code was verified by conducting a laboratory experiment.…”
Section: Introductionmentioning
confidence: 99%
“…6 This program utilizes the thin shocklayer approximations of Maslen 7 of computing either adiabatic (no heat loss) or nonadiabatic (radiation coupling) results. Both options were exercised, but only, the adiabatic results, which yield higher electron number densities than the nonadiabatic results, are presented.…”
Section: Inviscid Wakementioning
confidence: 99%
“…Extensive research on the topic was conducted in the late sixties [6,35,70,83,209] and early seventies [42,47,49,48,55,124,128,188]. These early efforts were motivated by a certain number of upcoming deep space exploration missions, including Apollo, Pioneer Venus Multiprobe (1978), and Galileo (launched in 1989).…”
Section: Radiative Couplingmentioning
confidence: 99%
“…The mission designers were aware of those limitations and applied a liberal margin of safety in the heat shield thickness. Some of them can be consulted chronologically in [140,48,180,129].…”
Section: E4 Numerical Studies E41 Pre-flight Of Pioneer Venusmentioning
confidence: 99%