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(19)

(11)

2 539 709

(13)

(51)

IPC

F42B15/00(2006-01-01)

F42B15/01(2006-01-01)

F42B10/60(2006-01-01)

F42B10/62(2006-01-01)

F42B10/64(2006-01-01)

(21) (22)

Application

2014101679/11, 2014-01-22

(24)

Start date

2014-01-22

(22)

Actual filing date

2014-01-22

(45)

Published

2015-01-27

(72)

Inventor

Bogatskij Vladimir Grigor'EvichKravchuk Aleksandr PavlovichLevishchev Oleg NikolaevichOreliov Grigorij RafailovichSmirnov Anatolij Georgievich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Mashinostroitel'Noe Konstruktorskoe Bjuro Imeni I.I. Toropova"

CONTROLLED MISSILE Russian patent published in 2015 - IPC F42B15/00 F42B15/01 F42B10/60 F42B10/62 F42B10/64

Abstract RU 2539709 C1

FIELD: weapons and ammunition.

SUBSTANCE: invention relates to missile engineering, namely to controlled missiles. A controlled missile includes a housing with the main control elements symmetrically arranged on it - aerodynamic surfaces and rudders, as well as a wire duct. The latter is arranged along the housing in the incline of rudders. An aerodynamic surface is additionally installed on the housing, on the side opposite to the wire duct.

EFFECT: improvement of aerodynamics of missile flight and improvement of its target guidance accuracy.

2 cl, 1 dwg

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RU 2 539 709 C1

Authors

Bogatskij Vladimir Grigor'Evich

Kravchuk Aleksandr Pavlovich

Levishchev Oleg Nikolaevich

Oreliov Grigorij Rafailovich

Smirnov Anatolij Georgievich

Dates

2015-01-27—Published

2014-01-22—Filed