The shuttle avionics integration laboratory (SAIL) requirements for supporting the Spacelab/orbiter avionics verification process are defined. The principal topics are a Spacelab avionics hardware assessment, test operations center/electronic systems test laboratory (TOC/ESL) data processing requirements definition, SAIL (Building 16) payload accommodations study, and projected funding and test scheduling. Because of the complex nature of the Spacelab/orbiter computer systems, the PCM data link, and the high rate digital data system hardware/software relationships, early avionics interface verification is required. The SAIL is a prime candidate test location to accomplish this early avionics verification.


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    Title :

    Space Shuttle Engineering and Operations Support. Avionics System Engineering


    Contributors:
    P. A. Broome (author) / R. J. Neubaur (author) / R. T. Welsh (author)

    Publication date :

    1976


    Size :

    62 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Space shuttle engineering and operations support. Avionics system engineering

    Broome, P. A. / Neubaur, R. J. / Welsh, R. T. | NTRS | 1976



    Space shuttle avionics system

    Hanaway, John F. / Moorehead, Robert W. | NTRS | 1989


    Space Shuttle Avionics System

    J. F. Hanaway / R. W. Moorehead | NTIS | 1989


    Space shuttle orbiter avionics

    Carrier, L.M. / Minor, R.G. | Tema Archive | 1977