vaz-raket1BR_57m1

AIRCRAFT ROCKETS 57 mm

The rockets are used to annihilate air targets at altitudes of up to 30.000 m , for assault actions against mobile and stationary armoured targets such as tanks , armoured vehicles , carriers , light weapon and vehicles , aircrafts on the ground and personnel around the stated combat means.

 

vazraket2BR_GRUP_MALA

We produce three types of these rockets:

> Aircraft Rocket BR-1-57 mm

BR -1- 57 rocket projectile is the Rocket of high explosive effect, 57 mm caliber and assembled with impact fuze, type UTI-1.

> Aircraft Rocket BR-2-57 mm

Rocket BR-2-57 is launched with the UTI-2 fuze from the launcher tube ( with the opened rear ends ) which is assembled in honeycomb rocket package.

> Aircraft Rocket BR-20-57 mm

The aircraft rocket of a hollow -charge and fragmentation effect BR-20-57 P1 is a system of Cal.57 mm unguided air-to-ground and air- to-air rockets and is used for mass arming of aircrafts.

The rocket includes a warhead with hollow charge and fragmentation effect and impact type UTI-2 fuze and superquick-inertial action.

S-8_KOMUNITED AVIATION ROCKETS 80 mm S-8 KOM

Unguided aviation rocket S-8 KOM with hollow-charge and fragmentation warhead of impact effect is intended to defea t armoured and unprotected targets on the ground as well as enemy′s personnel and is used for arming of aircrafts and helicopters.

The rockets are launched separately or in burst mode from twenty-tube launchers of honeycomb shape placed under the wings of aircraft (B-8M1) or under the helicopter arming carrier (B-8v20-a).

THE ROCKET CHARACTERISTICS
Caliber …………………………………………… 80 mm
Rocket mass …………………………………… 11,5 kg
Rocket length ……………………………… 1566 mm
Rocket penetration ……………………….. 350 mm
Temperature range of use …….. +50 do -60°C
Rocket velocity ……………………………… 610 m/s
Launching distance …………….1300 do 4000 m

VZ128mmM15AIRCRAFT ROCKETS 128 mm M15

BR-VZ-128 M15 is intended for operation at surface targets on the ground.

TECHNICAL DATA
Length ………………………………………… 1806 mm
Caliber ………………………………………….. 128 mm
Wingspar ……………………………………… 260 mm
Mass …………………………………………. 49-50,5 kg
Rocket maximum velocity ……………….600 m/s
Rocket engine operating time …………….. 1,2 s
Maximum range …………………………………10 km
Fragmentation effect radius ……………….. 25 m
Temperature range of use ……… +40 do -50°C

 

 

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>> Aircraft rockets BR-57 mm