The Spacelab side of the electrical interface between Spacelab subsystem equipment and experiments is presented. The electrical hardware which interfaces with the experiments is defined and the signal/load characteristics are stated. Major subsystems considered include: electrical power and distribution; command and data management subsystem; orbiter avionics via dedicated connectors of Spacelab; and electrical ground support equipment.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Spacelab payload accommodation handbook. Appendix A: Avionics interface definition


    Erscheinungsdatum :

    01.07.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch