Miniature missile
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United States of America Patent
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Mar 4, 2014
Grant Date -
Dec 23, 2010
app pub date -
Aug 16, 2007
filing date -
Aug 16, 2006
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Abstract
A miniature lightweight high-maneuverability missile (10) has a missile body (12) with three sets of at least two aerodynamic control surfaces (14, 16, 18) for independent control of roll, pitch and yaw of the missile. Each set of control surfaces (14, 16, 18) is independently controlled by a corresponding actuator (20) deployed within the missile body (12). Other preferred features include selection of an elevation angle of incidence at a target, and switching between explosive and kinetic modes of operation.
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