FIELD: rocketry, in particular, salvo-fire jet projectile systems, applicable in armament of rocket-artillery units of ground forces. SUBSTANCE: the jet projectile has a warhead and a solid fuel powder charge. The projectile rocket body is made with elongation of more than 10 calibers and wall thickness not exceeding 0.15% of its length. The projectile tail fins consists of a cylindrical cone and opening blades installed on it. The cylindrical cone is positioned in the lowering of the rocket body. The distance between the center of mass of the blades relative to the front end of the lowering of the rocket body does not exceed the preset value. EFFECT: enhanced fixing range with preservation of stability of motion in the whole flight trajectory. 3 dwg
Title | Year | Author | Number |
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JET PROJECTILE | 2000 |
|
RU2166179C1 |
SPIN-STABILIZED SUPERSONIC MISSILE | 2000 |
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RU2166178C1 |
SUPERSONIC JET PROJECTILE | 2001 |
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JET PROJECTILE | 2002 |
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ROCKET | 1998 |
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RU2150080C1 |
ROCKET PROJECTILE | 1999 |
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MISSILE UNIT OF JET PROJECTILE | 2003 |
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TAIL PLANE STABILIZER OF SUPERSONIC JET PROJECTILE | 2001 |
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RU2176066C1 |
ROCKET PROJECTILE LAUNCHED FROM LAUNCHING TUBE | 1997 |
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RU2115882C1 |
SALVO-FIRE JET PROJECTILE ELONGATED BY MORE THAN 20 CALIBERS | 1998 |
|
RU2150081C1 |
Authors
Dates
2003-06-27—Published
2002-02-12—Filed