It is shown that most promising systems are separate or integral storage type, utilizing water and ammonia as expendable coolants; operation of several control schemes presenting breadth of choice available between minimum refrigerant consumption and minimum of controls and complexity; methods of solving problems posed by weightlessness, high acceleration loading, installation and ground handling; recommendations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Approach to equipment cooling problems in orbital space vehicle


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Tupper, J.S. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1958 Cooling



    Erscheinungsdatum :

    1958


    Format / Umfang :

    18 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Problems of Environmental Testing of Orbital and Space Vehicle Structures

    Rathke, C. W. / Mayer, O. F. | SAE Technical Papers | 1966


    Medical problems in orbital space flight

    Strughold, H. | Engineering Index Backfile | 1956



    Space-based orbital transfer vehicle

    Charhut, D.E. / Ketchum, W.J. | Elsevier | 1986