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.


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    Title :

    Approach to equipment cooling problems in orbital space vehicle


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1958 Cooling



    Publication date :

    1958


    Size :

    18 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :



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