The objective of the Space Acceleration Measurement System (SAMS) is to measure and record the microgravity environment for a given experiment aboard the Space Shuttle. To accomplish this, SAMS uses remote triaxial sensor heads (TSH) that can be mounted directly on or near an experiment. The errors of the TSH are reduced by calibrating it before and after each flight. The associated error budget for the calibration procedure is discussed here.


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    Title :

    Space acceleration measurement system triaxial sensor head error budget


    Contributors:

    Publication date :

    1992-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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