SA-7 GRAIL 9K32M Strela-2
HN-5 (Hongying 5) China
Anza MKI - Pakistan
Ayn as Saqr - Egypt
| Specifications | |
|---|---|
| Date of Introduction | 1972 |
| Proliferation | Worldwide |
| Crew | 1 |
| Launcher Name | 9P54M |
| Length (m) | 1.47 |
| Diameter (mm) | 70 |
| Weight (kg) | 4.71 |
| Reaction Time | 5-10 seconds (acquisition to fire) |
| Time Between Launches (sec) | INA |
| Reload Time (sec) | 6-10 |
| Missile Name | 9M32M |
| Max. Range | 5,500 meters |
| Min. Range | 500 meters |
| Max. Altitude | 4,500 meters |
| Min. Altitude | 18 meters |
| Length (m) | 1.40 |
| Diameter (mm) | 70 |
| Weight (kg) | 9.97 |
| Missile Speed (m/s) | 580 |
| Propulsion | Solid fuel booster and solid fuel sustainer rocket motor. |
| Guidance | Passive IR homing device (operating in the medium IR range) |
| Seeker Field of View | 1.9° |
| Tracking Rate | 6°/sec |
| Warhead Type | HE |
| Warhead Weight (kg) | 1.15 |
| Fuze Type | Contact (flush or grazing) |
| Self-Destruct (sec) | 15 |
| FIRE CONTROL | Launcher has sighting device and a target acquisitionindicator. The gunner visually identifies and acquires the target. |
| Gunner Field of View | INA |
| Acquisition Range (m) | INA |
| VARIANTS |
SA-N-5 Naval version HN-5A Chinese version Strela 2M/A Yugoslavian upgrade Sakr Eye Egyptian upgrade Mounted in several types of vehicles in four, six, and eight-tube launcher varieties. Can be mounted on several helicopters (Mi-24, S-342 Gazelle) |
ANZA MK-1 Specifications | ||
|---|---|---|
| ||
| Type | 2-stage, low altitude | |
| Length | (missile, with retracted tail fins) 1.44 m | |
| Weight | (total launch assembly in firing condition) 15 Kg (Missile at launch) 9.8 Kg | |
| Propulsion | solid fuel booster and solid fuel sustainer rocket motor | |
| Guidance | uncooled Pbs passive infrared homing seeker | |
| Warhead | HE fragmentation (containing 0.37 Kg HE) with contact and graze fuzing | |
| Average missile cruise speed | 500 m/s | |
| Max missile manoeuvring | 6 g | |
| Self destruction time | 14-17 s | |
| Max target speed | (receding target) 260 m/s | |
| Max effective slant range | 4,200 m | |
| Min effective slant range | 1,200 m | |
| Max effective altitude | 50 m | |
| Weapon reaction time | less than 5 s | |
| Time from march to ready | less than 10 s for operation | |
| Battery operation time | more than 40 s | |
General characteristics
Parameter / Version PLØS |
STRELA-2 (SA-7A) | STRELA-2M (SA-7B) |
| Max. effective range | 3200 m | 4200 m |
| Max. effective ceiling | 2000 m | 2300 m |
| Min. altitude | 50 m | 30-50 m |
| Min. effective range | 800 m | 800 m |
| Max. speed of the target | 220 m/s | 260 m/s |
| Max. speed | 385 m/s | 580 m/s |
| Operating wavelength of the detector | 1,7 az 2,8 m m | 1,7 az 2,8 m m |
| Viewing field of the homing system | 1,9° | . |
| Angular scan velocity in the regime of target tracking | 9°/s | . |
| Total weight of the system | 14,5 kg | 15 kg |
| Weight of the missile | 9,2 kg | 9,85 kg |
| Weight of the warhead | 1,15 kg | 1,8 kg |
| Length of the missile | 1,42 m | 1,44 m |
| Diameter of the missile | 0,072 mm | 0,072 mm |
| Wingspan of the stabilisation wings | 300 mm | 300 mm |
| Length of the launcher | 1,49 m | 1,49 m |
| Diameter of the launcher | 0,1 m | 0,1 m |
| Into-action time | max. 6 s | . |
| Reaction time | max. 5 s | . |
| Time for self-destruction of the missile | 14 az 17 s | . |
| Range of operation temperatures | -38 az +50°C | . |
| Operator | 1 | 1 |
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