The approach used to integrate the thermal and life support systems of several large spacecraft is presented. These spacecraft will be assembled in earth orbit to make up the Apollo Applications Program (AAP) Orbital Assembly (OA). Due to the size of the spacecraft and the complexity of the systems involved, it was necessary to analyze the thermal and life support systems by defining appropriate interfaces and integrating the results into overall system math models.


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    Title :

    Environmental Control of Apollo Applications Program Orbital Assembly


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1969



    Publication date :

    1969-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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