This 10 month program derived the conceptual design of a small diameter, shoulder launched, direct fire missile for use as a guidance test bed. The resulting design is practical, versatile, and modular, and can exercise a variety of present and advanced technology seekers over a broad range regime. Although the missile makes maximum use of off-the-shelf components and is well within existing technology capabilities, its accuracy potential is sufficient for any anticipated guidance system.


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    Title :

    Terminal Homing Guidance for the Shoulder Launched Direct Fire Missile


    Contributors:
    R. C. Scott (author)

    Publication date :

    1975


    Size :

    184 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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