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At a glance
Hatf-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
Length
Single source6.0 m (19.7 ft)[source]
Length
Single sourceConfiguration
| Specification | Hatf-I | RS-24 Yars |
|---|---|---|
| Type | Short-range ballistic missile[source] | Intercontinental Ballistic Missile[source] |
| Place of origin | Pakistan[source] | Russia[source] |
| In service | 1992 –Present[source] | 2010–present[source] |
| Used by | Pakistan Army Air Defense Corps (1992–99) Air Defense Command (1999-2000) Army Strategic Forces Command (2000–Present)[source] | Russian Strategic Missile Troops |
22,500 mm[source]
Maximum; Maximum speed
Single source5.9–6.1 m/s (19–20 ft/s)[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]
Maximum; Maximum firing range
Single sourceOperational; Hatf-I
Single sourceOperational; Hatf-IA/IB
Single source100 km (62 mi)[source]
Hatf-I: 70 km (43 mi) Hatf-IA/IB: 100 km (62 mi)[source]
Operational; Operational range
Single source11,000 km (6,800 mi) - 12,000 km (7,500 mi)[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.
| Designer | Space Research Commission (Rocket system) Kahuta Research Laboratories (Warhead design/assembly)[source] | Moscow Institute of Thermal Technology[source] |
|---|
| Designed | 1987–89[source] | — |
|---|
| Manufacturer | Space Research Commission[source] | Votkinsk Machine Building Plant[source] |
|---|
| Produced | 1987–2001[source] | 2009[source] |
|---|
| No. built | 105 (stock estimated in 2021) )[source] | — |
|---|
| Variants | Hatf-I: 1992 Hatf-IA: 1995 Hatf-IB: 2001[source] | — |
|---|
| Warhead | Conventional HE / CE[source] | 3 x 200 kiloton MIRV warheads[source] |
|---|
| Engine | Single-stage[source] | Three-stage Solid-fuel rocket[source] |
|---|
| Payload capacity | 500 kg (1,100 lb)[source] | — |
|---|
| Transmission | Manual[source] | — |
|---|
| Suspension | M35 / Isuzu x 4WD semi-trailer[source] | — |
|---|
| Propellant | Solid-propellant[source] | — |
|---|
| Guidance system | Unguided :Hatf-I/IA Inertial : Hatf-IB[source] | Inertial with Glonass[source] |
|---|
| Accuracy | 100 m (330 ft) CEP[source] | — |
|---|
| Launch platform | Transporter erector launcher[source] | Silo , road-mobile TEL MZKT-79221[source] |
|---|