GUIDED MISSILE Russian patent published in 2005 - IPC

Abstract RU 2257535 C1

FIELD: armament.

SUBSTANCE: the guided missile has a body with an exposed afterbody, aerodynamic control members and a stabilizer in the form of flexible shortened cantilevers folding on the side surface of the missile body. The stabilizer cantilevers have an elliptic shape, in plan whose front and rear edges are determined by a definite dependence.

EFFECT: enhanced aeroballistic and strength characteristics of the missile.

4 dwg

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RU 2 257 535 C1

Authors

Shipunov A.G.

Zakharov L.G.

Morozov V.I.

Kopylov Ju.D.

Gusarov N.I.

Dates

2005-07-27Published

2004-06-28Filed