Raytheon Company

Hughes Aircraft Company

Donald P Williams

Robert W Adams

Wayne V Spate

Russell E Denker

A missile nose is tiltable and rotatable relative to a missile body through the action of an actuator system. In an exemplary embodiment, the actuator systems uses two electro-mechanical actuators mounted co-axially and having the output shaft of one actuator fed through the shaft of the other. One of the actuators controls a tilt angle between a longitudinal axis of the body and a longitudinal axis of the nose. The other actuator rotates the nose about the longitudinal axis of the body. A method of steering a missile includes using the actuator system to maintain the missile nose pointed at a target or other desired destination.

Articulated nose missile control actuation system

A container of a pressurized gas has an elongated inlet/outlet tubular neck which extends into a housing passage. A cap sealed over the inlet/outlet neck has a platelike member connected to the neck via a hollow support or column. A piston is slidingly received within the housing passage for movement toward the platelike member and has a rod which can be brought into contact with the member eccentrically of the hollow support. A squib on being discharged driving the piston toward the platelike member and rod cantilevers about the hollow support causing it to break and release the gas for use.

Growing community of inventors

Tucson, AZ, United States of America

Donald P Williams