The possibility of standard low temperature detector(s) for use in upcoming cryogenically cooled satellite and Space Shuttle Payloads was investigated. These payloads operate from .3 Kelvin to 300 Kelvin. Standard detectors were selected and matching signal conditioning equipment were specified. This equipment will operate in a spacecraft environment and be compatible with the selected detector, typical spacecraft voltages, typical spacecraft telemetry systems, and the radiation encountered by a typical earth orbiting spacecraft. Work statements to better define and advance detector performance are presented.


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    Title :

    Survey Report on the State-of-the-Art of Cryogenic Thermometry and Signal Conditioners and Their Potential for Standardized Space Hardware


    Publication date :

    1978


    Size :

    86 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English