A missile includes a tail section having a multi-nozzle grid with both fixed nozzlettes, and movable, thrust vector nozzlettes. The movable nozzlettes may be configured in a number of discrete array bars, each containing multiple of the movable nozzlettes. Movement of one or more array bars may be used to vector the thrust of the missile, providing roll, yaw, or spinning of the missile, for example.

 
Web www.patentalert.com

< Angular rate sensor using micro electromechanical haltere

< Penetrator and method of using same

> Aircraft engine rear suspension with thrust recovery

> More aerodynamic wheel fairings for small airplanes

~ 00285