GUIDED MISSILE Russian patent published in 2015 - IPC F42B15/00 F42B15/01 

Abstract RU 2542692 C1

FIELD: weapons and ammunition.

SUBSTANCE: guided missile is made based on canard configuration. The missile with a single-channel control system and rotating in roll direction. The missile contains a main propulsion system, a steering wheel in one plane and a stabiliser with the location of fixed bearing surfaces by X-shaped pattern relating to the plane of the steering wheel console. At the head part of the housing of the guided missile in a plane perpendicular to the plane of the steering wheel console, the pylons are mounted. The fixed consoles of the pylons in a transverse plane are located at an angle of 45-60 degrees relative the consoles of the stabiliser. The consoles of the pylon on the geometric shape in the plan are made like consoles of the steering wheel with the ratio of areas of the pylon and the steering wheel as 0.5-1.0. The ratio of areas of the console of the pylon and the console of the stabiliser are made as 0.05-0.1.

EFFECT: improved control efficiency, improved ballistic and dynamic properties of the missile.

2 dwg

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RU 2 542 692 C1

Authors

Zakharov Lev Grigor'Evich

Morozov Vladimir Ivanovich

Kopylov Jurij Dmitrievich

Golomidov Boris Aleksandrovich

Gusarov Nikolaj Ivanovich

Dates

2015-02-20Published

2014-02-03Filed