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BBallistic missiles
Medium-range ballistic missile (Agni-I, Agni-II, Agni Prime) Intermediate-range ballistic missile (Agni-III, Agni-IV) Intercontinental ballistic missile (Agni-V, Agni VI)
Measured figures
Agni-I
Single sourceAgni-II
Single sourceConfiguration
| Specification | 1KR1 Sapsan | Agni (missile) |
|---|---|---|
| Speed | Mach 7 (1.5 mi/s; 2.4 km/s)[source] | 24 Mach (Agni-V)[source] |
| Type | Tactical ballistic missile[source] | Medium-range ballistic missile (Agni-I, Agni-II, Agni Prime) Intermediate-range ballistic missile (Agni-III, Agni-IV) Intercontinental ballistic missile (Agni-V, Agni VI)[source] |
| Place of origin | Ukraine[source] | India[source] |
| In service | 2025–present[source] |
Agni-III
Single sourceAgni-IV
Single sourceAgni-P
Single sourceAgni-V
Single source15 m (Agni-I) 21 m (Agni-II) 17 m (Agni-III) 20 m (Agni-IV) 17.5 m (Agni-V) 10.5 m(Agni-P)[source]
Agni-I, Agni-II
Single sourceAgni-III, Agni V
Single sourceAgni-IV
Single sourceAgni P
Single sourceAgni VI
Single source1.0 m (Agni-I, Agni-II) 1.2 m(Agni-IV) 2.0 m (Agni-III, Agni V) 1.1 m (Agni VI) 1.15 m (Agni P)[source]
Agni-I
Single sourceAgni-II
Single sourceAgni III
Single sourceAgni-IV
Single sourceAgni P
Single sourceAgni-V
Single sourceAgni VI
Single source12,000 kg (Agni-I) 16,000 kg (Agni-II) 50,000 kg (Agni III) 17,000 kg (Agni-IV) 50,000 kg (Agni-V) 55,000 kg (Agni VI) 11,000 kg (Agni P)[source]
Operational; Operational range · source measurement 1
Single sourceOperational; Operational range · source measurement 2
Single sourceOperational; Operational range · source measurement 3
Single source50 km (31 mi) – 400–500 km (250–310 mi); 300 km (190 mi)[source]
Operational; Agni-I
Single sourceOperational; Agni-II
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Active[source]
| Used by | Ukrainian Ground Forces[source] | India[source] |
|---|
| Manufacturer | KB Pivdenne[source] | Bharat Dynamics Limited[source] |
|---|
| Warhead | 500 kg (1,100 lb)[source] | Conventional high explosive -unitary, penetration, cluster munitions , incendiary weapon , thermobaric , strategic nuclear weapon[source] |
|---|
| Engine | Single-stage solid propellant[source] | Composite rocket motor[source] |
|---|
| Designer | — | Defence Research and Development Organisation[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight altitude | — | 300 km (Agni-I) 230 km (Agni-II), 350 km (Agni-III)[source] |
|---|
| Guidance system | — | Mid-course: Ring laser gyro inertial navigation system with GPS / NavIC satellite guidance Terminal: Imaging infrared homing , radar scene correlation, active radar homing[source] |
|---|
| Launch platform | — | Road/Rail mobile[source] |
|---|
Operational; Agni-III
Single sourceOperational; Agni-IV
Single sourceOperational; Agni Prime
Single sourceOperational; Agni-V
Single sourceOperational; Agni VI
Single source700–1,200 km (Agni-I) 1,000–2,000 km (Agni Prime) 2,000–3,500 km (Agni-II) 3,000–5,000 km (Agni-III) 3,500–4,000 km (Agni-IV) 7,000–8,000 km (Agni-V) 11,000–12,000 km (Agni VI)[source]