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(19)

(11)

2 468 327

(13)

(51)

IPC

F41G7/22(2006-01-01)

(21) (22)

Application

2011146276/12, 2011-11-15

(24)

Start date

2011-11-15

(22)

Actual filing date

2011-11-15

(45)

Published

2012-11-27

(72)

Inventor

Gusev Andrej ViktorovichKuznetsov Vladimir MarkovichSel'Kin Vladislav VladimirovichPodchufarov Jurij BorisovichZakharov Oleg Vladimirovich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Bjuro Priborostroenija"

METHOD OF LAUNCHING MISSILE WITH LASER SEMI-ACTIVE-GUIDANCE HEAD Russian patent published in 2012 - IPC F41G7/22

Abstract RU 2468327 C1

FIELD: weapons and ammunition.

SUBSTANCE: topographical lock-on of launcher is effected with the help of satellite navigation system prior to setting the fire parameters. Fire control board with digital radio communication means is located 50-100 metres from launcher. Lock-on errors may not exceed 50 metres. Fire control parameters are transmitted in binary code to launcher ACS and, further, to missile. Launcher is turned to azimuth and elevation to launch the missile by command from control board.

EFFECT: increased range of fire, higher safety.

1 dwg

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RU 2 468 327 C1

Authors

Gusev Andrej Viktorovich

Kuznetsov Vladimir Markovich

Sel'Kin Vladislav Vladimirovich

Podchufarov Jurij Borisovich

Zakharov Oleg Vladimirovich

Dates

2012-11-27—Published

2011-11-15—Filed