Of conceivable vehicle configurations for nonlifting entry into earth's atmosphere shapes considered are -- spheres, spherical segments, and sphere-cones; total weight of entry vehicle was divided into structure, heat protection system (ablative material and insulation), and payload; equations and computational methods for shapes consisting of spherical segments, and for sphere cone shapes for which computer program, entry vehicle synthesis was used; comparison of sphere cone and spherical segment configurations.


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    Titel :

    Non-lifting entry-vehicle design for superorbital velocities


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Ambrosio, A. (Autor:in) / Baer, D.H. (Autor:in) / Myer, H.G. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Heat-Shield Ablation at Superorbital Re-Entry Velocities

    E. P. BARTLETT / W. E. NICOLET AND J. T. HOWE | AIAA | 1971


    Heat-shield ablation at superorbital re-entry velocities

    BARTLETT, E. / HOWE, J. / NICOLET, W. | AIAA | 1970


    Apollo ablator thermal performance at superorbital entry velocities

    Curry, Donald M. / Stephens, Emily W. | TIBKAT | 1970