The side thruster is a highly responsive means for attitude control of missiles. The sidejet force is influenced by the interaction of the sidejet with the external airflow. The sidejet aerodynamic interaction effects were analyzed from following two viewpoints: 1) the pressure field in the vicinity of the sidejet and 2) the force acting on the missile. Technical data of sidejet aerodynamic interaction effects were obtained by means of flight tests of missiles that were equipped with four impulse side thrusters that were small-size, rapidly burning solid-propellant rocket motors. The data agree with computational fluid dynamics analyses and wind-tunnel tests.


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    Title :

    Sidejet aerodynamic interaction effects of the missile


    Additional title:

    Auswirkungen eine seitlich austretenden Triebwerksstrahls auf die Aerodynamik eines Lenkflugkörpers


    Contributors:
    Kikumoto, K. (author) / Sentoh, E. (author) / Tanaka, H. (author) / Takahashi, T. (author)

    Published in:

    AIAA Journal ; 39 , 4 ; 611-617


    Publication date :

    2001


    Size :

    7 Seiten, 20 Bilder, 1 Tabelle, 8 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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