Advantages and limitations of five approaches for thermal design of spacecraft that do not involve testing entire prototype in space chamber with solar simulation for complete vehicle; fifth approach, thermal-scale modeling, which is considered in detail, offers advantages over others in that smaller models can be placed within existing solar-simulation beams, chamber-size demands are not great, and larger models can be used for limited number of applications; definition and requirements of scale model; modeling techniques and associated problems; uses and advantages of scale models.


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    Titel :

    Thermal scale modeling


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Thermal scale modeling.

    Vickers, J. M. F. | NTRS | 1965


    Limitations in thermal scale modeling

    MACGREGOR, R. K. | AIAA | 1971


    Thermal Scale Modeling of Spacecraft

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


    Thermal scale modeling of multilayered insulation

    FARMER, R. A. / SHIH, C. | AIAA | 1970


    Thermal scale modeling of spacecraft -- Experimental investigation

    Fowle, A.A. / Gabron, F. / Vickers, J.M.F. | Engineering Index Backfile | 1964