Missile
Type: single-stage, low- to high-altitude
Length
(S-200) 10.5 m
(S-200V) 10.8 m
(S-200D) 10.8 m
Diameter: 0.86 m
Max span: 2.85 m
Launch weight: (S-200V) 7,018 kg, (S-200D) 7,100 kg
Propulsion: four solid fuel strap-on boosters with liquid dual-thrust rocket motor
Guidance: command and/or active radar terminal homing seeker
Warhead: 217 kg (97 kg explosive) HE fragmentation with proximity and command fuzing optional 25 kt nuclear for nuclear warhead variants
Missile velocity range: 700-2,500 m/s
Max range:
(S-200) 150 km
(S-200V) 250 km
(S-200D) 300 km
Min range: 7 km
Max altitude:
(S-200) 20,000 m
(S-200V) 29,000 m
(S-200D) 40,000 m
Min altitude: 300 m
Launcher: static semi-fixed single rail trainable
Max target velocity: 1,180 m/s (head-on), 300 m/s (tail chase)
Deployment time: 24 min
Close-down time: 13 min