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Application

98115222/02, 1998-08-06

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Start date

1998-08-06

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Actual filing date

1998-08-06

(45)

Published

1999-08-10

(72)

Inventor

Arkhangel'Skij I.I.Belobragin V.N.Borisov O.G.Denezhkin G.A.Makarovets N.A.Mizrokhi V.Ja.Popov A.N.Svetlov V.G.Filippov V.S.Kuksa A.Ju.

(73)

Holder

Mashinostroitel'Noe Konstruktorskoe Bjuro Im.Akad.P.D.Grushina

JET PROJECTILE Russian patent published in 1999 - IPC

Abstract RU 2134400 C1

FIELD: salvo-fire artillery jet systems. SUBSTANCE: projectile uses a control system, warhead, rocket engine and an aerodynamic stabilizer. The stabilizer is furnished with bearings, whose axis is aligned with the projectile axis. The control system and stabilizer are linked with the opposite bearing races and mounted for mutual turning around the projectile axis. The distance between the bearings makes up 0.01 to 0.02 of the projectile length, and their rolling diameters - 0.45 to 0.85 of the projectile caliber. EFFECT: enhanced accuracy of fire. 3 dwg

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RU 2 134 400 C1

Authors

Arkhangel'Skij I.I.

Belobragin V.N.

Borisov O.G.

Denezhkin G.A.

Makarovets N.A.

Mizrokhi V.Ja.

Popov A.N.

Svetlov V.G.

Filippov V.S.

Kuksa A.Ju.

Dates

1999-08-10—Published

1998-08-06—Filed