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At a glance
Ghadr-110larger figure on 0 of 2
RS-24 Yarslarger figure on 2 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | Ghadr-110 | RS-24 Yars |
|---|---|---|
| Type | MRBM[source] | Intercontinental Ballistic Missile[source] |
| Place of origin | Iran[source] | Russia[source] |
| Used by | Iran[source] | Russian Strategic Missile Troops[source] |
| Manufacturer | Iran[source] | Votkinsk Machine Building Plant[source] |
22,500 mm[source]
Maximum; Mach 25 (
Single sourceMaximum; Maximum speed · source measurement 2
Single sourceMaximum; Maximum speed · source measurement 3
Single sourceMach 25 (30,600 km/h; 19,000 mph; 8,510 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Warhead | One[source] | 3 x 200 kiloton MIRV warheads[source] |
|---|
| Engine | First stage liquid, Second stage solid[source] | Three-stage Solid-fuel rocket[source] |
|---|
| Guidance system | Inertial guidance , Global Positioning System[source] | Inertial with Glonass[source] |
|---|
| Accuracy | CEP: 30-50m[source] | — |
|---|
| In service | — | 2010–present[source] |
|---|
| Designer | — | Moscow Institute of Thermal Technology[source] |
|---|
| Produced | — | 2009[source] |
|---|
| Launch platform | — | Silo , road-mobile TEL MZKT-79221[source] |
|---|
| Reported operators |
| — |
|---|