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2 229 668

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IPC

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Application

2003100216/02, 2003-01-04

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Start date

2003-01-04

(22)

Actual filing date

2003-01-04

(45)

Published

2004-05-27

(72)

Inventor

Bashkirov L.G.Demidov A.V.Kapustin V.A.Kaufman G.V.Kajumzhij V.N.Pigin E.A.Sokiran V.I.Solntsev S.V.

(73)

Holder

Oao Nauchno-Issledovatel'Skij Institut Priborostroenija Im. V.V. Tikhomirova Moskovskaja Obl., G. Zhukovskij, Ul. Gagarina,

FIRING SECTION Russian patent published in 2004 - IPC

Abstract RU 2229668 C1

FIELD: military equipment, in particular, mobile antiaircraft missile systems. SUBSTANCE: the firing section has an installation with a brightening and guidance radar comprising a series-connected multifunctional radar, digital computer system, data receiving-transmitting equipment, the third input of the digital computer system is connected to the output of the navigation, topographical survey and orientation system, the fourth input is connected to the output of the data measuring and input equipment, and the output of the data receiving-transmitting equipment of the installation with the brightening and guidance radar is connected to the input of the data receiving-transmitting equipment of the launcher, and a launcher comprising a series-connected data receiving-transmitting equipment, digital computer system, rotatable launcher, K antiaircraft guided missiles, the third input of the digital computer system is connected to the output of the navigation, topographical survey and orientation system, and the fourth input is connected to the output of the data measuring and input equipment, in addition, a phase radio rangefinder of brightening and guidance from the launcher is used, the responder of the phase rangefinder is located in the installation with the brightening and guidance radar, the interrogator of the phase rangefinder is located in the launcher, the input of the responder is connected to the output of the interrogator, the output of the responder is connected to the input of the interrogator, and the second output of the interrogator is connected to the fifth input of the digital computer system of the launcher. EFFECT: enhanced precision of generation of guidance signals for the antiaircraft guided missile due to the enhanced precision of measurement of the range between the installation and the launcher brightening and guidance radar. 3 dwg

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RU 2 229 668 C1

Authors

Bashkirov L.G.

Demidov A.V.

Kapustin V.A.

Kaufman G.V.

Kajumzhij V.N.

Pigin E.A.

Sokiran V.I.

Solntsev S.V.

Dates

2004-05-27—Published

2003-01-04—Filed