Mission requirements and constraints of 2-stage booster and spacecraft; both stages are manned, and employ lifting-entry configurations and current technologies to gain recoverable and reusable form; trajectory parameters including conditions of velocity, acceleration, altitude, and dynamic pressure are shown; propulsion system; aerodynamic and structural configuration, Astro performance and summary of structural design criteria and materials characteristics; recovery system; logistics and ground support, launch cost comparison and cost summary for 100 flights. (formerly Astronautics and Aerospace Eng)


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    Titel :

    Astro concept


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:
    Root, M.W. (Autor:in) / Fuller, G.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    ASTRO-D

    G. W. Ousley / Y. Tanaka | NTIS | 1991


    ASTRO-SPAS

    Senechal, Martin | Online Contents | 1994


    ASTRO-D

    Ousley, G. W., Sr. / Tanaka, Y. | NTRS | 1991


    Astro-navigation

    Mieville, A.L. | Engineering Index Backfile | 1942