Missile having non-cylindrical propulsion section

Details Missile having non-cylindrical propulsion section Missile having non-cylindrical propulsion section

F - Mech Eng,Light,Heat,Weapons

42

B

F42B 15/01 (2006.01) F42B 15/10 (2006.01)

Patent

CA 2183279

A missile (20) has a non-cylindrical fuselage (22b) over at least a portion of its length, with a non-cylindrical propulsion system (34) contained within the non-cylindrical portion (22b) of the fuselage. The fuselage (22b) and propulsion system (34) are preferably generally elliptical in cross section, with a dimensional ratio of the major axis to the minor axis of from more than 1:1 to about 1.5:1. The missile (20) further includes a guidance system (38) and control features (32).

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