Design concept of winged type vehicle, developed by Lockheed California Co is based on "hot structure", which depends on radiation for keeping temperature below maximum safe limits; material selected was Rene 41, using skin-corrugation type of surface structure, particularly CALAC configuration; main features of structure are illustrated; test specimen fabrication and material studies; structure and fatique testing.


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    Titel :

    Lightweight structures for space vehicles


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Childers, M.G. (Autor:in) / Koriagin, V.B. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Design



    Erscheinungsdatum :

    1961


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Lightweight Structures for Space Vehicles

    Milford, G. Childers / Koriagin, V. B. | SAE Technical Papers | 1961


    Lightweight inflatable shadow shields for cryogenic space vehicles

    Jones, L.R. / Barry, D.G. | Engineering Index Backfile | 1966


    Achieving lightweight vehicles; Designing and achieving lightweight vehicles

    Society of Automotive Engineers | British Library Conference Proceedings | 2002