MISSILE Russian patent published in 2015 - IPC F42B15/00 

Abstract RU 2548957 C1

FIELD: weapons and ammunition.

SUBSTANCE: missile includes case in the form of connected separable joint units with pyrotechnical burst connection of sealed head compartment with a sequence of homing head, inertial control system, ammunition, active thermal protection system and independent fluid or paste fuel propeller containing fuel with oxidiser and liquid-propellant rocket engine set with longitudinal nozzle, four liquid-propellant rocket engines with transverse nozzles and four liquid-propellant rocket engines generating head compartment torque, and propeller compartment with aerodynamic rudders, rudder drives, double-pulse solid fuel propeller aggregate, second pulse timing unit, correction unit.

EFFECT: efficient striking of high-altitude targets.

3 cl, 4 dwg

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RU 2 548 957 C1

Authors

Bogatskij Vladimir Grigor'Evich

Smirnov Anatolij Georgievich

Oreliov Grigorij Rafailovich

Mynkin Vladimir Aleksandrovich

Dates

2015-04-20Published

2014-05-15Filed