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At a glance
Prahaar (missile)larger 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
Operational; Pragati
Single sourceOperational; Prahaar
Single sourceOperational; Pranash
Single source150 km (93 mi) (Prahaar) 170 km (110 mi) (Pragati) 200 km (120 mi) (Pranash)[source]
Operational; Operational range
Single source11,000 km (6,800 mi) - 12,000 km (7,500 mi)[source]
Warhead weight
Single source250 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Prahaar (missile) | RS-24 Yars |
|---|---|---|
| Type | Tactical ballistic missile[source] | Intercontinental Ballistic Missile[source] |
| Place of origin | India[source] | Russia[source] |
| Designer | Defence Research and Development Organisation[source] | Moscow Institute of Thermal Technology[source] |
| Manufacturer | Bharat Dynamics Limited[source] | Votkinsk Machine Building Plant[source] |
| Warhead | High explosives , cluster munition[source] | 3 x 200 kiloton MIRV warheads[source] |
| Engine | Single-stage rocket motor[source] | Three-stage Solid-fuel rocket[source] |
| Propellant | Solid fuel[source] | — |
| Flight altitude | 35 km (22 mi)[source] | — |
| Guidance system | Mid-course: FOG - INS + multi- GNSS Terminal: ARH[source] | Inertial with Glonass[source] |
| Accuracy | 10 m (33 ft) CEP[source] | — |
| Launch platform | Tatra - BEML / Tata TEL[source] | Silo , road-mobile TEL MZKT-79221[source] |
| In service | — | 2010–present[source] |
| Used by | — | Russian Strategic Missile Troops[source] |
| Produced | — | 2009[source] |