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2 197 710

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IPC

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Application

2001128812/02, 2001-10-25

(24)

Start date

2001-10-25

(22)

Actual filing date

2001-10-25

(45)

Published

2003-01-27

(72)

Inventor

Shipunov A.G.Kuznetsov V.M.Komissarenko A.I.Rodin L.A.

(73)

Holder

Gosudarstvennoe Unitarnoe Predprijatie Bjuro Priborostroenija"

METHOD OF LAUNCH OF GUIDED ROCKET WITH OPTICAL TELEGUIDANCE AND ROCKET FOR ITS REALIZATION Russian patent published in 2003 - IPC

Abstract RU 2197710 C1

FIELD: rocket armament. SUBSTANCE: guided rocket with optical teleguidance is launched first with use of prelaunch engine of low thrust by light signal-flame with subsequent separation. Further direction finding is carried out by light signal from short- pulse radiation source installed in nozzle part of main boost engine and subsequent direction finding is conducted by light signal-flame of main boost engine while it is activated on flight trajectory and in boost of rocket to terminal calculated speed. Method is realized with the aid of guided rocket comprising sustainer stage with functional units and boost stage. Boost stage is fitted with prelaunch engine of low thrust and short- pulse source of light radiation mounted in nozzle part of main boost engine. Outer surface of membrane of main boost engine is brilliant to enhance light signal. EFFECT: increased reliability of control over rocket with optical teleguidance during its launch. 5 cl, 2 dwg

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RU 2 197 710 C1

Authors

Shipunov A.G.

Kuznetsov V.M.

Komissarenko A.I.

Rodin L.A.

Dates

2003-01-27—Published

2001-10-25—Filed

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