Launcher chassis type

wheel-type, with high cross-country ability

Amount of missiles on launcher

1

Total mass of mobile launcher, t

19

?perating temperature range, °?

from –40 to +50

Rocket

single-stage, solid-propellant, controllable, with
controllable head-separated at active phase end

Control system

autonomous, inertial, interconnected with satellite navigation system user terminal and homing head

Main propulsion system

solid-propellant with charge of mixed solid propellant of HTPB type, cocoon-type shell, rotated control nozzle

Launch type

pop-up launch out of TLC by means of cartridge pressure accumulator

Mass of missile, kg:

launch

3 300

with TLC

4 440

Mass of head, kg

480

Range, km:

maximum

up to 500 km

280 [for export]

minimum

55

Fuel mass, kg

2 250

Rocket length, m

6.4

Rocket diameter, m

0.924