JET PROJECTILE Russian patent published in 2001 - IPC

Abstract RU 2166179 C1

FIELD: rocketry. SUBSTANCE: jet projectile has a jet engine, made in the length within 1.8-3 of the caliber before the stabilizing fin with reduction, and its diameter makes up 0.7-0.8 of the projectile caliber. The stabilizing fin fairing has a diameter of 0.9-1.0 of the caliber and is provided with a tapered adapter connecting it to the jet engine. The adapter length equals 0.3-0.6 of the caliber. The projectile nose is connected to the jet engine through a tapered flare, having a length of 0.5-1.0 of the projectile caliber, and the blade span of the stabilizing fin corresponds to the relation given in the claim. EFFECT: enhanced aerodynamic power of the stabilizing fin, enhanced relative coordinate of the center of gravity, and as result, enhanced flight stability and reliability of projectile functioning. 1 dwg

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RU 2 166 179 C1

Authors

Gilik G.B.

Ivanov A.N.

Denezhkin G.A.

Makarovets N.A.

Ignatenko A.V.

Semilet V.V.

Peturkin D.M.

Filatov V.G.

Obozov L.I.

Bazarnyj A.N.

Batov A.G.

Sidjakov V.S.

Aljazhedinov V.R.

Borisova V.M.

Pygin A.F.

Dates

2001-04-27Published

2000-06-26Filed