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2 125 704

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C1

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IPC

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Application

98103790/02, 1998-03-16

(22)

Actual filing date

1998-03-16

(45)

Published

1999-01-27

(72)

Inventor

Belobragin V.N.Borisov O.G.Gushin V.A.Denezhkin G.A.Petrov V.L.Makarovets N.A.Obozov L.I.Semilet V.V.

(73)

Holder

Gosudarstvennoe Nauchno-Proizvodstvennoe Predprijatie

ROCKET Russian patent published in 1999 - IPC

Abstract RU 2125704 C1

FIELD: rocket engineering. SUBSTANCE: invention is related to rockets ( rocket missiles ) of rocket systems ( complexes ) of salvo firing fitted predominantly with stabilization systems. Rocket has warhead, mechanism opening (separating ) warhead with actuator, mechanism counting opening time of warhead and acceleration transmitter. Mechanism counting opening time of warhead has capability of presetting of specified opening time of warhead before start and is fitted with adder. Unit computing corrections of opening time of warhead is placed between adder and acceleration transmitter and realizes algorithm of type of Tp=TTp= Tp.t+ΔT+TpT, where Tp is time of opening of warhead; Tp.t is preset time of opening of warhead; ΔT - is correction to opening time of warhead. Acceleration transmitter, unit computing correction of opening time of warhead, adder, mechanism counting opening time and mechanism opening warhead are intercoupled electrically. Output of acceleration transmitter is connected through unit computing corrections of opening time of warhead to adder. Output of adder is coupled to mechanism opening warhead. Acceleration transmitter is located at distance of 8-12 calibers and actuator of mechanism opening warhead at distance not more than one caliber from center of mass of rocket. EFFECT: improved density of hits. 2 dwg

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RU 2 125 704 C1

Authors

Belobragin V.N.

Borisov O.G.

Gushin V.A.

Denezhkin G.A.

Petrov V.L.

Makarovets N.A.

Obozov L.I.

Semilet V.V.

Dates

1999-01-27—Published

1998-03-16—Filed

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