An unmanned air vehicle for military, land security and the like operations includes a fuselage provided with foldable wings having leading edge flaps and trailing edge ailerons which are operable during ascent from launch to control the flight pattern with the wings folded, the wings being deployed into an open unfolded position when appropriate. The vehicle is contained within a pod from which it is launched and a landing deck is provided to decelerate and arrest the vehicle upon its return to land.

 
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< MINE-DEFEATING SUBMUNITION

> IN-SITU AND EX-SITU ELECTROPHORESIS-BASED FORMATION OF ALIGNED NANOSTRUCTURE TRIGGERS FOR SOLID EXPLOSIVES

> SMART FUZE GUIDANCE SYSTEM WITH REPLACEABLE FUZE MODULE

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