Tail unit for a missile

Details Tail unit for a missile Tail unit for a missile

F - Mech Eng,Light,Heat,Weapons

02

K

60/67, 244/1.5

F02K 9/00 (2006.01) F42B 10/16 (2006.01)

Patent

CA 1079077

TAIL UNIT FOR A MISSILE ABSTRACT OF THE DISCLOSURE This invention provides a tail unit for a missile which is propelled at supersonic speed. The tail unit includes at least two pairs of curved blades, of which one of the longitudinal edges is connected to the periphery of a cylindrical body. The tail unit is rotated in flight with each blade being pivoted about a pivot pin integral with the cylindrical body. The length of the circular arc defined by the transverse profile of a blade is between 25% and 50% of the length of the periphery of a cross-section of the cylindri- cal body, wherein the orientation of the concavity of the blades of one and the same pair of blades about the axis of the cylindrical body is opposite to that of the blades of the other pair of blades. The blades can be folded down onto one another pearwise parallel to the outer surface of the body by rotation about the pivot pins.

280991

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