FORCETALLY
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Measured figures
Configuration
| Specification | Ababeel (missile) | RS-24 Yars |
|---|---|---|
| Type | MIRV surface-to-surface missile ballistic missile[source] | Intercontinental Ballistic Missile[source] |
| Place of origin | Pakistan[source] | Russia[source] |
| In service | 2017 –Present[source] | 2010–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces Command )[source] |
Height
Single source21.5 m (71 ft)[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]
3-8 MIRVs 3 Warheads of each (standard) 5 Warheads of
Single sourceeach
Single sourceeach 8 Warheads of
Single source3-8 MIRVs 3 Warheads of 500kg each (standard) 5 Warheads of 300kg each 8 Warheads of 185kg each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russian Strategic Missile Troops[source] |
| Designed | 2010–2017[source] | — |
|---|
| Manufacturer | National Engineering & Scientific Commission (NESCOM)[source] | Votkinsk Machine Building Plant[source] |
|---|
| Warhead | HE / NE[source] | 3 x 200 kiloton MIRV warheads[source] |
|---|
| Blast yield | >50 kilotons of TNT (210 TJ)[source] | — |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | WS21200 16WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-fuel[source] | — |
|---|
| Guidance system | Inertial , Terminal[source] | Inertial with Glonass[source] |
|---|
| Launch platform | Transporter erector launcher (TEL), Launch pad[source] | Silo , road-mobile TEL MZKT-79221[source] |
|---|
| Designer | — | Moscow Institute of Thermal Technology[source] |
|---|
| Produced | — | 2009[source] |
|---|
| Engine | — | Three-stage Solid-fuel rocket[source] |
|---|