Comparisons of equilibrium temperature measurements of prototype and three scaled thermal models of simulated spacecraft made within "cold-wall" vacuum chamber form basis of investigation; 1/2-and 1/5-scale model of prototype were tested to examine applicability of set of thermal modeling laws which specifies different materials of construction to achieve identical temperatures at homologous locations in model and prototype; third model, also 1/2-scale, was tested to examine application of another set of thermal modeling laws which allows use of identical materials but predicts different temperature fields in model and prototype; summary of results obtained.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thermal scale modeling of spacecraft -- Experimental investigation


    Weitere Titelangaben:

    AIAA -- Tech Paper


    Beteiligte:
    Fowle, A.A. (Autor:in) / Gabron, F. (Autor:in) / Vickers, J.M.F. (Autor:in)

    Kongress:

    Meeting of the AIAA -- Space Simulation Testing Conference ; 1964 Testing



    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    THERMAL SCALE MODELING OF SPACECRAFT - AN EXPERIMENTAL INVESTIGATION

    FOWLE, A. / GABRON, F. / VICKERS, J. | AIAA | 1964


    Thermal scale modeling of spacecraft - An experimental investigation.

    Fowle, A. A. / Gabron, F. / Vickers, J. M. F. | NTRS | 1966



    Thermal scale modeling of spacecraft - an experimental investigation.

    Fowle, A. A. / Gabron, F. / Vickers, J. M. F. | NTRS | 1964


    Thermal Scale Modeling of Spacecraft

    Shannon, R. L. / Klockzien, V. G. | SAE Technical Papers | 1969