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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    Titel :

    Environmental Control of Apollo Applications Program Orbital Assembly


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1969



    Erscheinungsdatum :

    01.02.1969




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Apollo lunar orbital science.

    Roberson, F. I. / Esenwein, G. F. | NTRS | 1972



    Apollo applications program requirements

    Rambaut, P. C. | NTRS | 1970


    Lunar orbital rendezvous for Apollo

    Holmes, D.B. | Engineering Index Backfile | 1963