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Application

2002118521/02, 2002-07-09

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Start date

2002-07-09

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Actual filing date

2002-07-09

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Published

2003-12-20

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Inventor

Aljazhedinov V.R.Belobragin V.N.Borisov O.G.Denezhkin G.A.Kaljuzhnyj G.V.Makarovets N.A.Semilet V.V.Sidorov E.V.

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

JET PROJECTILE Russian patent published in 2003 - IPC

Abstract RU 2219484 C1

FIELD: jet projectiles provided mainly with cluster warheads. SUBSTANCE: the projectile has a control system unit with an acceleration transducer and a separation connector, warhead with its break-down mechanism and a missile unit with a guide pin. The acceleration transducer is rigidly coupled to the control system unit mounted with a clearance fit and fixed on the main frame the missile unit. The deviation of the angle of turn of the plane passing through the axis of the separation connector and the projectile longitudinal axis relative to the plane passing through the axis of the guide pin and the projectile longitudinal axis does not exceed 0.035 radian. EFFECT: enhanced efficiency of target hitting. 4 dwg

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RU 2 219 484 C1

Authors

Aljazhedinov V.R.

Belobragin V.N.

Borisov O.G.

Denezhkin G.A.

Kaljuzhnyj G.V.

Makarovets N.A.

Semilet V.V.

Sidorov E.V.

Dates

2003-12-20—Published

2002-07-09—Filed

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