The scaling relations presently derived illustrate the influence of ballistic coefficient and L/D primary vehicle parameters on the peak heating rate and total heating/unit area for gliding entry of the earth atmosphere at parabolic speed. Comparisons with stagnation-point and windward centerline laminar and turbulent heating during three Space Shuttle flights are presented. It is found that total heat input/unit area is reduced by decreasing both of the primary vehicle parameters.


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    Titel :

    Scaling relations for heating during gliding entry at parabolic speed


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.12.1986



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Speed in gliding

    Neilan, J.C. | Engineering Index Backfile | 1951