A dual structure aerospace vehicle is described which has an aeroshell structure and an internally disposed separable and reusable integral tank/thrust structure. The tank/thrust structure is inuslated for cryogenic fuels and the cavity within aeroshell is insulated from the tank/thrust structure. An internal support ring within the cavity serves as an attachment for lugs on the tank/thrust structure via double hinges. The aft end of tank/thrust structure is provided with rocket engines and exit nozzles with a trunnion supporting the tank/thrust structure within the aeroshell.


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    Titel :

    Aerospace vehicle


    Beteiligte:
    Jackson, L. R. (Autor:in) / Taylor, A. H. (Autor:in)

    Erscheinungsdatum :

    1985-12-10


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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