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122 MM MISSILE LAUNCHER - 26.400 DFAEG (6X6)

Loading: 12.0 (t)

ROMAN
Missile launcher vehicle, all-wheel drive 6x6,single tires front and rear, permanently coupled, high performance on non-level ground, designed to remote launching of 122 mm rocket missiles. It can launch 40 GRAD missiles/ 20 sec at a distance of 45 km or 26 LAR Mk4 missiles in 45 sec. The cab room is provided for 5+1 persons. It is interface provided;. It is transportable on the railroad and C130H plane. Operated with NATO fuel.
Produs
PERFORMANCES
Maximum speed90.0 Km/h
Longitudinal slope25.0 %
Cross slope15.0 %
Turning diameter between curbs23.6 m
Rake angle30.0 °
30.0 °
Temperature range-33…52 C
QR
DIMENSIONS AND WEIGHTS
Permissible total weight23000.0 kg
Overall length8540.0 mm
Total width2500.0 mm
Total height loaded (unloaded)3100.0 mm
Ground clearance front (back)400.0 mm
BODY
    It has the capacity of launching both standard missiles of 160 mm from the launcher with 26 launching tubes arranged in 2 tactic containers having the future potential of launching also rockets with Accular trajectory correction One LAROM launcher can launch 40 GRAD missiles in 20s or 26 LAR Mk. 4 missiles in 45s. Each LAR missile scatters 104 bomb lets on a circular area having diameter of 200 m. The system also contains modern artillery control system (ACCS) attending all artillery units and all ammunition types. The tactic computer (GTAC, FTAC or ATAC) has a state-of-the-art man-vehicle interface that reduces the crew efforts enabling an easy and fast actuation of main targeting and shooting controls and that of the launcher ammunition system as well. It also allows a computerized feed-back reaction for corrections between launcher, the front observatory and the point of command. The firing control unit is to be actuated from the cab or from a nearby shelter by means of a remote control provided with a 50 m long cable. The launcher has an individual firing option as well as that of automatic partial or complete firing with a variable rate (repetition frequency) in 4 stages between 0,5 s and 1,8 s. At a firing rate of 1,8 s all the 26 missiles can be launched in 46,8 s.
EQUIPPING
ENGINE
TypeMAN D 2066 LF – 4 stroke, 6 cylinders in line, water-cooled, intercooling.
Displacement10.520 l
Rated power400 HP / 1900 rpm
Torque1900 Nm / 1000-1400 rpm
Level of pollutionEURO5
TRANSMISSION
ClutchType: F&S 430, single plate, dry,
GearboxType: 16S2220OD, mechanical synchromesh with 16 forward and two reverse gears. PTO NH/4C. Option : automatic transmission Allison
Distribution boxType: ZF VG2000, mechanical, permanently coupled, 2 gears, lockable interaxial differential
Front axleType: PF9, steering, drive axle.
Rear axleType: PT 13+PS13, tandem, drive axle with lockable differential.
CABINE
    Type: MGL, metallic, full forward control, flat windshield glass, heating and ventilation system, hatch on the roof, mirrors,special equipments. 4 seats and 2 doors, air conditioner system Ballistic protection bullet and antipersonnel mine. (level 1 – STANAG 4569)
WHEELS
Tires14.00 R 20 profile ON-OFF road - single front and rear - CTIS (Central Tire Inflation System)
BRAKES
Brake systemIntegral pneumatic with 2 independent circuits and ABS.
WINCH

SEPSON, hydraulic, 10 tons maximum force, rope length 50 m, front and rear drive

Romania, Brasov - 500419, 5 Poienelor st.
Sales department
Technical department