Propulsive torque motor
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United States of America Patent
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Nov 12, 2002
Grant Date -
N/A
app pub date -
Sep 11, 2000
filing date -
Oct 12, 1999
priority date (Note) -
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Abstract
A spin-stabilized missile includes two or more spin nozzles along a perimeter of the missile, the nozzles being operatively coupled to a pressurized gas source. The pressurized gas source provides pressurized gas which passes through the nozzles and external to the missile, thereby providing circumferential thrust which causes a torque on the missile that results in the missile rolling or spinning. The pressurized gas source may be a pressure container containing solid rocket fuel. The pressurized gas source for spinning the missile may be the same as that for the missile's main propulsion system.
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