Results of wind tunnel testing of three rocketsonde temperature sensors at reduced pressures are reported. These tests were performed to evaluate the effective aerodynamic recovery factor in rarefied flows simulating flight conditions experienced in rocketsonde flights between 50 and 70 km. (Author)


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    Title :

    Wind Tunnel Evaluation of High Altitude Temperature Sensors


    Contributors:

    Publication date :

    1968


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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