A five-stage solid-fuel sounding-rocket system which can boost a payload of 25 pounds to an altitude of 525 nautical miles and that of 100 pounds to 300 nautical miles is described. Data obtained from a typical flight test of the system are discussed.


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    Title :

    Five-Stage Solid-Fuel Sounding-Rocket System


    Contributors:

    Publication date :

    1959


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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