FORCETALLY
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At a glance
Fattah-2larger figure on 0 of 1
RS-24 Yarslarger 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 | Fattah-2 | RS-24 Yars |
|---|---|---|
| Type | Hypersonic missile[source] | Intercontinental Ballistic Missile[source] |
| Used by | Iran[source] | Russian Strategic Missile Troops[source] |
| Designer | IRGC engineers[source] | Moscow Institute of Thermal Technology[source] |
| Manufacturer | AIO[source] | Votkinsk Machine Building Plant[source] |
Diameter
Single source2,000 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 | Conventional Warhead[source] | 3 x 200 kiloton MIRV warheads[source] |
|---|
| Propellant | Stage 1: Solid‑Fuel Booster Stage 2: Liquid‑Fuel HGV[source] | — |
|---|
| Launch platform | Road‑mobile TEL[source] | Silo , road-mobile TEL MZKT-79221[source] |
|---|
| Country of origin | Iran[source] Iran[source] | — |
|---|
| Place of origin | — | Russia[source] |
|---|
| In service | — | 2010–present[source] |
|---|
| Produced | — | 2009[source] |
|---|
| Engine | — | Three-stage Solid-fuel rocket[source] |
|---|
| Guidance system | — | Inertial with Glonass[source] |
|---|