The unique problems encountered in the integrated approach to aircraft and spacecraft avionics system designs are discussed with the emphasis on recent advances in telemetry as a factor facilitating the integration. A listing of subsystems planned for integration on the Space Shuttle vehicle is given, covering auxiliary pumping and propellant, crew controls and displays, computation, communications and radar, electric power, guidance, navigation and control, air-bearing engines, main engines, reaction control, and structural/mechanical elements. Considerations are given for the multiplexed data bus design applicable to integrated avionics.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Telemetry and the integrated avionics approach.


    Contributors:
    Frost, W. O. (author) / Ellis, D. H. (author)

    Conference:

    Telemetry applications in the aerospace industry; Seventeenth International Aerospace Instrumentation Symposium ; 1971 ; Las Vegas, NV


    Publication date :

    1971-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




    Integrated avionics

    Online Contents | 1998


    Integrated Avionics

    Ford, Terry | Online Contents | 1994


    Integrated Avionics

    Ford, T. | British Library Online Contents | 1994