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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)
At a glance
Measured figures
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]
Mass
Single source31,000–32,000 kg (68,000–71,000 lb)[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; Operational range
Single source10,000 km (6,200 mi)[source]
(4.14 tf) (second stage)
Single sourceTwo-stage, liquid-fueled (48 tf) (first stage)
Single sourceTwo-stage, liquid-fueled 470 kN (48 tf) (first stage) 40.6 kN (4.14 tf) (second stage)[source]
Warhead weight
Single source300–500 kg (660–1,100 lb)[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-14 |
|---|---|---|
| Speed | 24 Mach (Agni-V)[source] | — |
| 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] | Intercontinental ballistic missile[source] |
| Place of origin | India[source] | North Korea[source] |
| In service | Active[source] | First successful test on 4 July 2017[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] | — |
| Engine | Composite rocket motor[source] | — |
| Propellant | Solid fuel[source] | UDMH/ N 2 O 4[source] |
| Flight altitude | 300 km (Agni-I) 230 km (Agni-II), 350 km (Agni-III)[source] | 3,720 km (2,310 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] | — |
| Launch platform | Road/Rail mobile[source] | Road-mobile TEL[source] |
| Produced | — | 2017–present[source] |
| No. built | — | Unknown[source] |
| Chosŏn'gŭl | — | 《화성-14》형[source] |
| Hancha | — | 火 星 14 型[source] |
| Revised Romanization | — | Hwaseong 14-hyeong[source] |
| McCune–Reischauer | — | Hwasŏng 14-hyŏng[source] |