Mercury man-in-space program involves ballistic type re-entry vehicle utilizing ablative and heat sink materials in its primary heat shield; basic reasons for trend toward lifting type re-entry, heat shield problems of these vehicles, role that ceramics may play in lifting vehicle radiative shields, and test on two ceramic materials.


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    Titel :

    Ceramic heat shields for glide re-entry vehicles


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Davis, R.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Heat problems



    Erscheinungsdatum :

    1961


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Ceramic Heat Shields for Glide Re-Entry Vehicles

    Davis, R. M. | SAE Technical Papers | 1961


    Ceramic Heat Shields for Lifting Re-entry Vehicles

    Krusos, James N. | SAE Technical Papers | 1968



    Ablative heat shields for planetary entry vehicles.

    Sparhawk, H. E. / Strauss, E. L. | NTRS | 1968


    Blunted-Cone Heat Shields of Atmospheric Entry Vehicles

    Button, Eleanor C. / Lilley, Charles R. / Mackenzie, Nicholas S. et al. | AIAA | 2009