The initial objective was to study the use of superplastically formed corrugated hat section stringers and frames in place of integrally machined stringers over separate frames for the tanks of large launch vehicles subjected to high buckling loads. The ALS was used as an example. The objective of the follow-on project was to study methods of designing shell structures subjected to severe combinations of structural loads and thermal gradients, with emphasis on new combinations of structural arrangements and materials. Typical applications would be to fuselage sections of high speed civil transports and to cryogenic tanks on the National Aerospace Plane.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of cryogenic tanks for space vehicles shell structures analytical modeling


    Beteiligte:
    Copper, Charles (Autor:in) / Mccarthy, K. (Autor:in) / Pilkey, W. D. (Autor:in) / Haviland, J. K. (Autor:in)


    Erscheinungsdatum :

    1991-06-30


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Design of Cryogenic Tanks for Space Vehicles Shell Structures Analytical Modeling

    C. Copper / K. Mccarthy / W. D. Pilkey et al. | NTIS | 1991


    Cryogenic Tanks for Launch Vehicles

    Nebiolo, M. / Basile, L. / Cramarossa, A. et al. | AIAA | 2004


    Cryogenic Pressure Control Modeling for Ellipsoidal Space Tanks

    Lopez, Alfredo / Grayson, Gary / Chandler, Frank et al. | AIAA | 2007


    Cryogenic Pressure Control Modeling for Ellipsoidal Space Tanks AIAA Paper

    Lopez, A. / Grayson, G. / Chandler, F. et al. | British Library Conference Proceedings | 2007


    Cryogenic Pressure Control Modeling for Ellipsoidal Space Tanks in Reduced Gravity

    Lopez, Alfredo / Grayson, Gary / Chandler, Frank et al. | AIAA | 2008