Determination of the stagnation region heating of probes entering the Venusian atmosphere. Both convective and radiative heat-transfer rates are predicted, and account is taken of the important effects of radiative transport in the vehicle shock layer. A nongray radiative transport model is utilized which parallels a four-band treatment previously developed for air (Page et al., 1969), but includes two additional bands to account for the important CO(4+) molecular band system. Some comparisons are made between results for Venus entry and results for earth entry obtained using a viscous earth entry program.


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    Titel :

    Radiative and convective heating during Venus entry.


    Beteiligte:
    Page, W. A. (Autor:in) / Woodward, H. T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1972-10-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Radiative and convective heating during Venus entry.

    PAGE, W. A. / WOODWARD, H. T. | AIAA | 1972


    Radiative and convective heating during atmospheric entry

    Rigdon, W. S. / Dirling, R. B. / Thomas, M. | TIBKAT | 1968


    Radiative and convective heating during hypervelocity re-entry

    NEREM, R. M. / STICKFORD, G. H. | AIAA | 1964