MULTIMISSION GUIDED MISSILE IN LAUNCHING PACK Russian patent published in 2006 - IPC F42B15/00 

Abstract RU 2277693 C1

FIELD: armament.

SUBSTANCE: the multimission guided missile in a launching pack has an acceleration engine, radio equipment package, cruise engine, controls section, gyroscopic sensor, as well as a replaceable warhead. The pack has two spaced in its length power trunnions for attachment to the carrier. Positioned in the first one is a pyrolock for holding the missile, and a switching for holding the missile, and a switching plate with two groups of contacts for successive connection to the power source on the carrier is mounted on the second one. A matching plate is installed on the launching pack. The switching terminal of starting current from the carrier to the starting circuit of the acceleration engine is installed in the front trunnion under the pyrolock, it is closed at actuation of the pyrolock.

EFFECT: enhanced opportunities of the missile, enhanced destructive action of it.

4 cl, 12 dwg

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RU 2 277 693 C1

Authors

Pitikov Sergej Viktorovich

Grishin Valerij Vasil'Evich

Kashin Valerij Mikhajlovich

Vukolov Aleksandr Sergeevich

Sudarikov Valerij Ivanovich

Batishchev Konstantin Aleksandrovich

Skrjabin Mikhail Aleksandrovich

Rjutin Valerij Borisovich

Pronchev Jurij Vasil'Evich

Shljakhov Valerij Pavlovich

Dates

2006-06-10Published

2004-09-23Filed