Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
RS-24 Yarslarger figure on 3 of 3
Sky Spearlarger figure on 0 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source22,500 mm[source]
Length
Single sourceConfiguration
| Specification | RS-24 Yars | Sky Spear |
|---|---|---|
| Type | Intercontinental Ballistic Missile[source] | Short-range ballistic missile[source] |
| Place of origin | Russia[source] | Taiwan[source] |
| In service | 2010–present[source] | 2001-current[source] |
| Used by | Russian Strategic Missile Troops[source] | — |
8.0 m[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.
| Designer |
|---|
Moscow Institute of Thermal Technology[source] |
National Chung-Shan Institute of Science and Technology[source] |
| Manufacturer | Votkinsk Machine Building Plant[source] | — |
|---|
| Produced | 2009[source] | — |
|---|
| Warhead | 3 x 200 kiloton MIRV warheads[source] | — |
|---|
| Engine | Three-stage Solid-fuel rocket[source] | — |
|---|
| Guidance system | Inertial with Glonass[source] | — |
|---|
| Launch platform | Silo , road-mobile TEL MZKT-79221[source] | Transporter erector launcher or silo[source] |
|---|
| No. built | — | Unknown[source] |
|---|
| Payload capacity | — | 500 kg[source] |
|---|
| Propellant | — | Two-stage solid propellant[source] |
|---|
| Transport | — | Truck[source] |
|---|