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.


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    Title :

    Spacelab Payload Accommodation Handbook. Appendix A: Avionics Interface Definition


    Publication date :

    1978


    Size :

    208 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English