A micro-unmanned aerial vehicle deployment system is provided for a cruise missile having submunition compartments. The system includes a vehicle launch module releasable from the cruise missile submunition compartment. The vehicle launch system has a control circuit and at least one micro-unmanned aerial vehicle contained therein. Structure is provided in the launch module for deploying the micro-unmanned aerial vehicle. A separable tether can be joined between the cruise missile and the vehicle launch module that separates when subjected to tension after deployment of the vehicle launch module.


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    Title :

    Micro-Unmanned Aerial Vehicle Deployment System


    Contributors:

    Publication date :

    2011


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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