FORCETALLY
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At a glance
Abdali-Ilarger figure on 0 of 3
RS-24 Yarslarger figure on 3 of 3
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]
Warhead weight
Single source500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Abdali-I | RS-24 Yars |
|---|---|---|
| Type | SRBM[source] | Intercontinental Ballistic Missile[source] |
| Place of origin | Pakistan[source] | Russia[source] |
| Used by | Pakistan Army Army Strategic Forces Command[source] | Russian Strategic Missile Troops[source] |
| Designer | SUPARCO (Rocket stage) DESTO (Warhead design/assembly)[source] | Moscow Institute of Thermal Technology[source] |
| Designed | 1993–97[source] | — |
| Manufacturer | SUPARCO[source] | Votkinsk Machine Building Plant[source] |
| Warhead | Single conventional HE / ICM[source] | 3 x 200 kiloton MIRV warheads[source] |
| Transmission | Automatic[source] | — |
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | — |
| Propellant | Solid-propellent[source] | — |
| Guidance system | Inertial , Terminal[source] | Inertial with Glonass[source] |
| Accuracy | 100 m (330 ft)—150 m (490 ft) CEP .[source] | — |
| Launch platform | Transporter erector launcher (TEL)[source] | Silo , road-mobile TEL MZKT-79221[source] |
| In service | — | 2010–present[source] |
| Produced | — | 2009[source] |
| Engine | — | Three-stage Solid-fuel rocket[source] |