MISSILE Russian patent published in 2004 - IPC

Abstract RU 2234667 C1

FIELD: rocketry; guided missiles with aerodynamic actuators.

SUBSTANCE: proposed missile is made according to standard aerodynamic configuration. It has body where engine, guidance equipment and control systems, fighting equipment, four fixed wings and four aerodynamic control surfaces are arranged. Wings and control surfaces are smoothly distributed relative to longitudinal axis of body.

EFFECT: enhanced maneuverability.

6 dwg

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RU 2 234 667 C1

Authors

Akimov V.N.

Bulgakova R.G.

Gol'Denberg A.M.

Kuvshinov E.M.

Ehktov V.P.

Dates

2004-08-20—Published

2002-11-18—Filed