FORCETALLY
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Measured figures
travelling
Single source7.95 m (26 ft 1 in) (travelling)[source]
travelling
Single source2.375 m (8 ft) (travelling)[source]
travelling
Single source2.25 m (7 ft 5 in) (travelling)[source]
travelling with ammunition
Single source7,400 kg (16,300 lb) (travelling with ammunition)[source]
per barrel
Single source800 rpm per barrel[source]
HEI ammunition
Single source1,035 m/s (3,400 ft/s) (HEI ammunition)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Artemis 30 | S-500 missile system |
|---|---|---|
| Type | Anti-aircraft system[source] | Mobile surface-to-air missile[source] |
| Place of origin | Greece[source] | Russian Federation[source] |
| Used by | Greece[source] | Russian Space Forces[source] |
| Designer | Anastasios Georgiou & Athanassios Calligeris, Ph.D.[source] | Almaz-Antey[source] |
| Designed | 1982[source] | — |
| Manufacturer | Hellenic Arms Industry[source] | Almaz-Antey[source] |
| Shell | Aluminium cased 30 mm x 173 mm[source] | — |
| Action | Gas operated[source] | — |
| Carriage | Four wheel twin axle split type with onboard generator[source] | — |
| Elevation | -5° to +85°[source] | — |
| Traverse | 360°[source] | — |
| Sights | On board gyroscopic 2D tracking sight[source] | — |
| In service | — | 16 September 2021[source] |
| Unit cost | — | $2.5 billion[source] |
| Produced | — | 2021–present[source] |
| No. built | — | 1 S-500 regiment in service[source] |
| Reported operators |
| — |