FORCETALLY
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At a glance
9K35 Strela-10larger figure on 0 of 1
S-500 missile systemlarger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | 9K35 Strela-10 | S-500 missile system |
|---|---|---|
| Type | Vehicle-mounted SAM system[source] | Mobile surface-to-air missile[source] |
| Place of origin | Soviet Union[source] | Russian Federation[source] |
| In service | 1976–present[source] | 16 September 2021[source] |
| Used by | See list of operators[source] | Russian Space Forces |
Width
Single source2,850 mm[source]
firing
Single sourcetravelling
Single source2,300 mm (travelling), 3,800 mm (firing)[source]
commander, gunner and driver
Single source3 (commander, gunner and driver)[source]
Maximum; road
Single sourceMaximum; water
Single source61.5 km/h (road) 6 km/h (water)[source]
YaMZ-238 V diesel
Single sourceYaMZ-238 V diesel 240 hp[source]
Warhead weight
Single source5 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Angolan Civil War Iran–Iraq War Persian Gulf War Afghan Civil War (1989–1992) Afghan Civil War (1992–1996) Kosovo War Syrian Civil War Russo-Ukrainian War Russo-Ukrainian war (2022–present) Second Nagorno-Karabakh War[source] | — |
|---|
| Designer | KB Tochmash Design Bureau of Precision Engineering[source] | Almaz-Antey[source] |
|---|
| Designed | 1969–1976[source] | — |
|---|
| Manufacturer | Saratovskiy Zenit Machine Plant (Muromteplovoz Joint Stock Company for the 9K35M3-K)[source] | Almaz-Antey[source] |
|---|
| Produced | 1976–present[source] | 2021–present[source] |
|---|
| Variants | Strela-10, Strela-10SV (Prototype), Strela-10M, Strela-10M2, Strela-10M3, Strela-10M3-K, Strela-10M4[source] | — |
|---|
| Armour | 7 mm[source] | — |
|---|
| Main armament | 4 × 9M333 (or 9M37MD)[source] | — |
|---|
| Secondary armament | 1x PKMB machine gun[source] | — |
|---|
| Suspension | torsion bar[source] | — |
|---|
| Ground clearance | 0.5 m[source] | — |
|---|
| Fuel capacity | 450 litres[source] | — |
|---|
| Warhead | Frag-HE[source] | — |
|---|
| Detonation mechanism | contact and laser proximity fuzes[source] | — |
|---|
| Propellant | single-stage solid propellant rocket motor[source] | — |
|---|
| Flight altitude | 3,500 metres (11,500 ft)[source] | — |
|---|
| Guidance system | dual-mode passive 'photocontrast'/IR seeker[source] | — |
|---|
| Unit cost | — | $2.5 billion[source] |
|---|
| No. built | — | 1 S-500 regiment in service[source] |
|---|
| Reported operators |
| — |
|---|