AAir defence
RIM-174 Standard ERAM
Surface-to-air missile (primary role) Anti-ballistic missile (terminal phase) Anti-ship missile (secondary role)
FORCETALLY
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AAir defence
Surface-to-air missile (primary role) Anti-ballistic missile (terminal phase) Anti-ship missile (secondary role)
Measured figures
Configuration
| Specification | RIM-174 Standard ERAM | S-500 missile system |
|---|---|---|
| Type | Surface-to-air missile (primary role) Anti-ballistic missile (terminal phase) Anti-ship missile (secondary role)[source] | Mobile surface-to-air missile[source] |
| Place of origin | United States[source] | Russian Federation[source] |
| In service | 2013–present[source] | 16 September 2021[source] |
| Used by | United States Navy Royal Australian Navy Japan Maritime Self Defense Force Republic of Korea Navy[source] |
Wingspan
Single source42.0 in (1.07 m)[source]
for Block IA
Single sourcefor Block IB
Single source13.5 in (0.34 m) for Block IA 21 in (0.53 m) for Block IB[source]
Maximum; 1.2 km/s
Single sourceMaximum; Mach 3.5 (
Single sourceMach 3.5 (2,664.2 mph; 4,287.7 km/h; 1.2 km/s)[source]
Operational; against land targets
Single sourceOperational; around
Single sourceOperational; or upwards of
Single source130 nmi (150 mi; 240 km) or upwards of 250 nmi (290 mi; 460 km) around 500 km against land targets[source]
Operational; Operational range
Single source600 km[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russian Space Forces[source] |
| Manufacturer | Raytheon[source] | Almaz-Antey[source] |
|---|
| Unit cost | US$4.87M (US$8,766.6M for 1800) US$4,318,632 (FY2021) (average)[source] | $2.5 billion[source] |
|---|
| Produced | 2009–present[source] | 2021–present[source] |
|---|
| No. built | 500 (1,800 planned)[source] | 1 S-500 regiment in service[source] |
|---|
| Warhead | 140 lb (64 kg) blast fragmentation[source] | — |
|---|
| Detonation mechanism | Radar and contact fuze[source] | — |
|---|
| Engine | Two stage: solid rocket booster, solid rocket booster/sustainer[source] | — |
|---|
| Flight ceiling | >110,000 ft (34,000 m)[source] | — |
|---|
| Guidance system | Inertial guidance , terminal active and Semi-active radar homing[source] | — |
|---|
| Launch platform | Mk 41 VLS (surface ship) Typhon missile system (ground launcher)[source] | — |
|---|
| Designer | — | Almaz-Antey[source] |
|---|