Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
RS-24 Yarslarger figure on 4 of 4
Shaurya (missile)larger figure on 0 of 4
Measured figures
Length
Single source22,500 mm[source]
Length
Single sourceConfiguration
| Specification | RS-24 Yars | Shaurya (missile) |
|---|---|---|
| Type | Intercontinental Ballistic Missile[source] | Short-range ballistic missile[source] |
| Place of origin | Russia[source] | India[source] |
| In service | 2010–present[source] | — |
| Used by | Russian Strategic Missile Troops[source] | Strategic Forces Command[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
10 m (33 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]
Maximum; 2.55 km/s
Single sourceMaximum; Mach 7.5 (
Single sourceWarhead weight
Single source200–1,000 kilograms (440–2,200 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
Moscow Institute of Thermal Technology[source] |
Research Centre Imarat[source] |
| Manufacturer | Votkinsk Machine Building Plant[source] | Bharat Dynamics Limited[source] |
|---|
| Produced | 2009[source] | 2011–present[source] |
|---|
| Warhead | 3 x 200 kiloton MIRV warheads[source] | Conventional and strategic nuclear weapon[source] |
|---|
| Engine | Three-stage Solid-fuel rocket[source] | Two-stage solid rocket motor[source] |
|---|
| Guidance system | Inertial with Glonass[source] | RLG - INS and accelerometer[source] |
|---|
| Launch platform | Silo , road-mobile TEL MZKT-79221[source] | Canisterised transporter erector launcher or underground silo[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight altitude | — | 50 km (31 mi)[source] |
|---|
| Accuracy | — | 20 m to 30 m CEP[source] |
|---|
| Reported operators | — |
|
|---|
Mach 7.5 (9,190 km/h; 5,710 mph; 2.55 km/s)[source]