A parametric analysis of a broad spectrum of thermostructural concepts is presented. A complete structural concept for the 35-foot entry test vehicle using the FDL-5 configuration is defined. Subsystems for the entry test vehicle are selected. A weight breakdown and a weight summary for the test vehicle are presented. (Author)


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    Titel :

    Preliminary Design and Experimental Investigation of the FDL-5A Unmanned High L/D Spacecraft. Part 5. Vehicle Design


    Beteiligte:
    P. P. Plank (Autor:in) / I. F. Sakata (Autor:in) / M. Verhaegh (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    134 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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