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Almaz S-200 Angara/Vega (SA-5 'Gammon') low- to high-altitude surface-to-air missile system
Description
Each S-200 missile battalion has one P-35M (NATO designation `Bar Lock-B') E/F-band 320 km range target search and acquisition radar with an integral D-band IFF system, one H-band (NATO designation `Square Pair') 270 km plus range missile guidance radar, and six trainable semi-fixed single rail 5P72 launchers with supporting loader units, prelaunch preparation cabins and diesel-powered electricity generator stations.
The missile itself is of the single-stage type with four jettisonable, wraparound solid fuel booster packs. Each booster is 4.9 m long, 0.48 m in diameter and has a single fin span length of 0.35 m from the booster body. The basic S-200 is 10.5 m long overall and has a maximum wing span of 2.85 m. The main body is 0.86 m in diameter and has a single stage liquid fuel 10,000 kg total thrust, 51-150 second duration rocket engine sustainer.
The minimum range of around 7 km is due to the 3-5 second, 160,000 kg thrust total duration booster burn time and jettison requirements which limit it to engagements against relatively large unmanoeuvrable targets at ranges up to the maximum of the missile model. Guidance beyond the 60 km booster jettison point is by course correction command signals from the `Square Pair' radar with the S-200's own active radar terminal homing seeker head being activated near to the projected intercept point for the final guidance phase. The large HE warhead is detonated either by a command signal or the onboard proximity fuzing system.
Specifications
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
Erklärung zum Bild:S-200 on its launcher (Photo: C F Foss)