The aerodynamic and mechanical design aspects and the performance analysis for the TATER rocket system are discussed. The TATER is a three-stage, solid-propellant rocket system capable of boosting a 70-lb recoverable payload to velocities of 10,500 to 11,000 ft/s in approximately 12 seconds from launch with a maximum velocity altitude variation of 10,000-30,000 ft on an ascent trajectory. (ERA citation 01:011224)


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    Title :

    Aeroballistic and Mechanical Design and Development of the Talos-Terrier-Recruit (Tater) Rocket System with Flight Test Results


    Contributors:

    Publication date :

    1976


    Size :

    120 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English