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
Title | Year | Author | Number |
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|
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SPIN-STABILIZED ROCKET | 2000 |
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ROCKET PROJECTILE WITH A GAS-DYNAMIC STABILIZATION SYSTEM | 2020 |
|
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Authors
Dates
2008-05-27—Published
2006-09-04—Filed