WINGED MISSILE (VERSIONS) Russian patent published in 2017 - IPC F42B15/00 

Abstract RU 2622274 C1

FIELD: weaponry and ammunition supplies.

SUBSTANCE: according to one version, winged missile contains the fuselage, wing, turbojet engine and few subammunitions, i.e. controlled or free-falling bombs. The computer of the missile guidance system provides a program of its flight over several targets in several passes. It is possible to select targets located approximately on a straight line. It provides a program for bombs free-falling from low altitudes with adjustment of their flight trajectory with a view to the release of the above bombs at a specified angle to the horizontal or down at a metered rate, or braking, depending on the type of the target. Another option includes two-axis gyrostabilized biplane radio direction finder and infrared biplane direction finder. In addition, there are bomb bays with two doors at the top and bottom and a bounding mechanism for the inside bomb bays of anti-radar and infrared missiles, which are subammunitions. There is also a release device for dropping subammunitions, i.e. missiles, down. When the stock of subammunitions is more than the number of hit targets, you can drop the subammunitions in the form of bombs. For the latter case there is a possibility of cutting off missile engines, keeping the missile controls in neutral, of unarmed position of non-contact detonators and armed position of non-contact detonators.

EFFECT: increased efficiency of hitting targets with a winged missile.

4 cl, 2 dwg

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RU 2 622 274 C1

Authors

Staroverov Nikolaj Evgenevich

Dates

2017-06-13Published

2016-02-24Filed