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ABallistic 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 sourceAgni-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]
estimated
Single source16.5 m (54 ft) (estimated)[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]
estimated
Single source1.5 m (4.9 ft) (estimated)[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]
24.7 tons (estimated)[source]
Operational; Agni-I
Single sourceOperational; Agni-II
Single sourceOperational; 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]
Operational; estimated
Single source3,700–6,000 km (2,300–3,700 mi) (estimated)[source]
Liquid-propellant rocket , single chamber variant of Paektusan 104,300 lb f
Single sourceLiquid-propellant rocket , single chamber variant of Paektusan 464.1 kN (104,300 lb f )[source]
estimated
Single source500–650 kg (1,100–1,430 lb) (estimated)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Agni (missile) | Hwasong-12 |
|---|---|---|
| Type | 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] | Intermediate-range ballistic missile[source] |
| Place of origin | India[source] | North Korea[source] |
| In service | Active[source] | 2017–present[source] |
| Used by | India[source] | Korean People's Army Strategic Force[source] |
| Designer | Defence Research and Development Organisation[source] | — |
| Manufacturer | Bharat Dynamics Limited[source] | North Korea[source] |
| Warhead | Conventional high explosive -unitary, penetration, cluster munitions , incendiary weapon , thermobaric , strategic nuclear weapon[source] | Conventional; possibly nuclear-capable[source] |
| Engine | Composite rocket motor[source] | — |
| Propellant | Solid fuel[source] | Hypergolic combination of unsymmetrical dimethylhydrazine (UDMH) as fuel, and either Dinitrogen tetroxide ( N 2 O 4 )[source] |
| Flight altitude | 300 km (Agni-I) 230 km (Agni-II), 350 km (Agni-III)[source] | 2,111.5 km (1,312.0 mi) (lofted trajectory)[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] | Inertial[source] |
| Launch platform | Road/Rail mobile[source] | MAZ-based vehicle[source] |
| Produced | — | June 2017[source] |
| Accuracy | — | greater than 5 km (3.1 mi) CEP[source] |
| Chosŏn'gŭl | — | 《화성-12》형[source] |
| Hancha | — | 火 星 十 二 型[source] |
| Revised Romanization | — | Hwaseong-12[source] |
| McCune–Reischauer | — | Hwasŏng-12[source] |
| Reported operators | — |
|