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.
Micro-Unmanned Aerial Vehicle Deployment System
2011
22 pages
Report
Keine Angabe
Englisch
UNMANNED AERIAL VEHICLE DEPLOYMENT PARAMETER MODIFICATION
Europäisches Patentamt | 2024
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