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IPC

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Application

2001107104/02, 2001-03-20

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Start date

2001-03-20

(22)

Actual filing date

2001-03-20

(45)

Published

2002-02-10

(72)

Inventor

Makarovets N.A.Denezhkin G.A.Semilet V.V.Obozov L.I.Aljazhedinov V.R.Ryleev S.P.Zakharov O.L.Kaljuzhnyj G.V.Podchufarov V.I.Tregubov V.I.Petrov V.L.Gushchin V.A.

(73)

Holder

Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

MISSILE Russian patent published in 2002 - IPC

Abstract RU 2179299 C1

FIELD: rocketry, in particular missiles (jet projectiles) with detachable nose cones, applicable in development of jet projectiles of salvo-fire systems. SUBSTANCE: in the missile, containing a rocket engine, detachable nose cone and a separation device with an actuator the separation device with an actuator, the separation device is made in the form of a launching tube installed on the engine, its length makes up at least 1.1 of the missile caliber, and the nose cone installed in a spaced relation in the launching tube is made with an equator moment of inertia not exceeding 0.1 of the equator moment of inertia of the missile, the value of the diametral clearance makes up 0.04 to 1.2% of the inside diameter of the launching tube. EFFECT: enhanced reliability of functioning, minimized level of disturbances imparted to the nose cone at separation, enhanced characteristics of close grouping of shots. 6 dwg

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RU 2 179 299 C1

Authors

Makarovets N.A.

Denezhkin G.A.

Semilet V.V.

Obozov L.I.

Aljazhedinov V.R.

Ryleev S.P.

Zakharov O.L.

Kaljuzhnyj G.V.

Podchufarov V.I.

Tregubov V.I.

Petrov V.L.

Gushchin V.A.

Dates

2002-02-10—Published

2001-03-20—Filed