Design considerations require knowledge of structural response to load and of launch loads which involves shell buckling, stress analysis, panel flutter, noise, vehicle response to horizontal winds, vibrations, dynamic modeling, and study of new configuration concepts; latter requires expanded viewpoint including more elements of vehicle system, fuel slosh, control frequency, and their relationship to lateral vibration modes; new concept of scalloped tank which provides baffling by means of radial webs which act also as structural tension members.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Research, design considerations, and technological problems of structures for launch vehicles


    Weitere Titelangaben:

    NASA -- Univ Conf Science Technology Space Exploration -- Proc


    Beteiligte:
    Runyan, H.L. (Autor:in) / Leonard, R.W. (Autor:in)

    Kongress:

    Proceedings of the NASA -- University Conference on Science and Technology of Space Exploration ; 1962 Design



    Erscheinungsdatum :

    1962


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Operational Considerations for Reusable Launch Vehicles

    Adelgren, R. G. / Ray, D. / Lashinski, P. et al. | British Library Conference Proceedings | 1997




    Aerodynamic problems of launch vehicles

    Boswinkle, Jr., R.W. | Engineering Index Backfile | 1962