SPINNING MISSILE Russian patent published in 2008 - IPC F42B15/00 F42B10/02 F42B12/02 

Abstract RU 2325612 C1

FIELD: weapons and ammunition.

SUBSTANCE: spinning missile comprises warhead with a cylindrical case containing a fluid filler and an air chamber and a rod being arranged on the spinning missile symmetry axis. The missile also comprises a missile aerodynamic stabilizer with canted fins and a gas-dynamic angular stabilization system with nozzles. The air chamber volume is from 0.2 to 0.05 of the cylindrical body volume, and the distance between the centre of mass of the spinning missile and the centre of mass of the warhead does not exceed a value determined by the given mathematical expression.

EFFECT: enhancement of fire engagement.

1 dwg

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RU 2 325 612 C1

Authors

Makarovets Nikolaj Aleksandrovich

Denezhkin Gennadij Alekseevich

Semilet Viktor Vasil'Evich

Kaljuzhnyj Gennadij Vasil'Evich

Belobragin Boris Andreevich

Shirokov Vladimir Vasil'Evich

Terekhov Bogdan Nikolaevich

Varenykh Nikolaj Mikhajlovich

Sporykhin Aleksandr Ivanovich

Dates

2008-05-27Published

2006-09-04Filed