Preparing your view.
ABallistic missiles
Rocket artillery Short-range ballistic missile Medium-range ballistic missile Anti-ship ballistic missile
At a glance
Precision Strike Missilelarger 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
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]
Maximum; ≥
Single source≥ 310 mi (500 km)[source]
more than 400 kilometers[source]Baseline missile / planned development performance stated in 2024 editionSource text · numeric interpretation needs review
Operational; Operational range
Single source11,000 km (6,800 mi) - 12,000 km (7,500 mi)[source]
Warhead weight
Single source200 lb (91 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Precision Strike Missile | RS-24 Yars |
|---|---|---|
| Type | Rocket artillery Short-range ballistic missile Medium-range ballistic missile Anti-ship ballistic missile[source] | Intercontinental Ballistic Missile[source] |
| Place of origin | United States[source] | Russia[source] |
| In service | 2023–present[source] | 2010–present[source] |
| Used by | United States Australia[source] | Russian Strategic Missile Troops[source] |
| Wars | 2026 Iran war[source] | — |
| Designer | Lockheed Martin Missiles and Fire Control[source] | Moscow Institute of Thermal Technology[source] |
| Unit cost | < $3.5 million (Increment One)[source] | — |
| Warhead | HE fragmentation blast Unknown number of submunitions Future iterations will possibly include Coyote drones and Hatchet miniature glide bombs from Northrop Grumman .[source] | 3 x 200 kiloton MIRV warheads[source] |
| Propellant | solid-propellant rocket[source] | — |
| Guidance system | Base: INS + GPS Land-based anti-ship missile: Base + anti-radiation seeker + Imaging Infrared (IIR)[source] | Inertial with Glonass[source] |
| Launch platform | M270 MLRS , M142 HIMARS , GMARS[source] | Silo , road-mobile TEL MZKT-79221[source] |
| Manufacturer | Lockheed Martin Missiles and Fire Control[source] | Votkinsk Machine Building Plant[source] |
| Launch platforms | M270A2 Multiple Launch Rocket System and the M142 High Mobility Artillery Rocket System[source]Unspecified by source | — |
| Produced | — | 2009[source] |
| Engine | — | Three-stage Solid-fuel rocket[source] |
| Reported operators |
| — |