The electronics and temperature sensing units of the pulse-to-pulse rocketsonde are described. The sonde is designed for the 2 1/8-inch dart of the SUPER-LOKI meteorological rocket. In flight, the sonde descends by parachute from rocket apogees of about 75 kilometers. As the sonde descends, it transmits air temperature data back to ground radio receiving stations.


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    Title :

    University of Utah four-channel pulse-to-pulse commutated SUPER-LOKI rocket meteorological parachutesonde (electronics)


    Contributors:
    Atwood, K. W. (author) / Soss, D. A. (author)

    Publication date :

    1976-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English