Principles employed in development of aerospace ground checkout and launch control equipment for use on Apollo and Gemini programs; PACE-S/C system is composed of PCM ground station subsystem, computing subsystem, display and control subsystem, data transmission subsystem, and spacecraft associated subsystem; details of each system and 3 modes of operation; primary method of real-time data display utilized is crt system which displays engineering data from computing complex in alphanumeric form.


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    Title :

    PACE -- Preflight acceptance checkout equipment


    Additional title:

    Astronautics Aerospace Eng


    Contributors:
    Parsons, W.E. (author) / Johnson, H.G. (author) / Woods, G.J. (author)


    Publication date :

    1963


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    PACE- PREFLIGHT ACCEPTANCE CHECKOUT EQUIPMENT

    Johnson, H. G. / Parsons, W. E. / Woods, G. J. | NTRS | 1963




    Preflight acceptance testing.

    Preston, G. M. | NTRS | 1964