ABallistic missiles
Agni-V
Intermediate-range ballistic missile Reported Intercontinental ballistic missile capability
FORCETALLY
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ABallistic missiles
Intermediate-range ballistic missile Reported Intercontinental ballistic missile capability
Measured figures
Configuration
| Specification | Agni-V | Oreshnik (missile) |
|---|---|---|
| Type | Intermediate-range ballistic missile Reported Intercontinental ballistic missile capability[source] | Intermediate-range ballistic missile[source] |
| Place of origin | India[source] | Russia[source] |
| In service | Active[source] | 2024–Present[source] |
| Used by | Strategic Forces Command[source] | Russia |
Diameter
Single source2 metres (6 ft 7 in)[source]
Mass
Single source50000–56000 kg[source]
Maximum; 8.17 km/s
Single sourceMaximum; Terminal phase: Mach 24 (
Single sourceTerminal phase: Mach 24 (29,400 km/h; 18,300 mph; 8.17 km/s)[source]
Maximum; 3.40 km/s
Single sourceMaximum; Over Mach 10 (
Single sourceair-burst or bunker buster
Single sourceWarhead weight
Single source3,000–4,000 kilograms (6,600–8,800 lb) 7,500–8,000 kilograms (16,500–17,600 lb) ( air-burst or bunker buster )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Defence Research and Development Organisation[source] | — |
|---|
| Manufacturer | Bharat Dynamics Limited[source] | — |
|---|
| Unit cost | ₹ 50 crore (US$5 million)[source] | Unknown[source] |
|---|
| Warhead | 3-6 (tested) 10-12 warheads Nuclear MIRVs[source] | Nuclear / conventional[source] |
|---|
| Engine | Three-stage solid rocket[source] | — |
|---|
| Propellant | Solid fuel[source] | — |
|---|
| Guidance system | RLG - INS + multi- GNSS + redundant micro-inertial navigation[source] | — |
|---|
| Launch platform | 8 × 8 Tatra TEL Rail Mobile Launcher (Canisterised Missile Package)[source] | — |
|---|
| Transport | Road[source] | — |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Designed | — | 2020s[source] |
|---|
| Developed from | — | RS-26 Rubezh[source] |
|---|
| Produced | — | 2024–Present[source] |
|---|
Over Mach 10 (12,300 km/h; 7,610 mph; 3.40 km/s)[source]