ABallistic missiles
Hyunmoo
Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile
FORCETALLY
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ABallistic missiles
Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile
Measured figures
Configuration
| Specification | Hyunmoo | Pralay (missile) |
|---|---|---|
| Type | Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile[source] | Tactical ballistic missile[source] |
| Place of origin | South Korea[source] | India[source] |
| In service | 1987–present[source] | — |
| Used by | Republic of Korea Armed Forces[source] | Indian Army Indian Air Force[source] |
Maximum; > Mach 4 (
Single sourceMaximum; Maximum speed
Single source> Mach 4 (3,045 mph ; 4,900 km/h )[source]
Maximum; 2.08 km/s
Single sourceMaximum; Mach 6.1 (
Single sourceWarhead weight · source measurement 1
Single sourceWarhead weight · source measurement 2
Single source350–700 kg (770–1,540 lb) 500–1,000 kg (1,100–2,200 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
Agency for Defense Development[source] |
Research Centre Imarat[source] |
| Manufacturer | Hanwha (Hyunmoo-2/4/5) LIG Defense & Aerospace (Hyunmoo-3)[source] | Bharat Electronics Bharat Dynamics Limited[source] |
|---|
| Produced | 1980s–present[source] | — |
|---|
| Variants | Hyunmoo-1 Hyunmoo-2A Hyunmoo-2B Hyunmoo-2c Hyunmoo-3A Hyunmoo-3B Hyunmoo-3C Hyunmoo-3D Hyunmoo-4 Hyunmoo-4.4 ( submarine version ) Hyunmoo-5 ( bunker buster )[source] | — |
|---|
| Warhead | Conventional[source] | HE PF , PCB , RDPS[source] |
|---|
| Payload capacity | 500 to 8,000 kg (1,100 to 17,600 lb)[source] | — |
|---|
| Propellant | solid fuel[source] | Solid[source] |
|---|
| Guidance system | command guidance[source] | Mid-course: INS Terminal: MMW DSMAC + Radar Imaging[source] |
|---|
| Launch platform | mobile launchers[source] | 12 x 12 Ashok Leyland HMV TEL[source] |
|---|
| Transport | KM1500[source] | — |
|---|
| Engine | — | Two stage rocket + MaRV[source] |
|---|
| Accuracy | — | <10 metres (33 ft) CEP[source] |
|---|
| Reported operators | — |
|
|---|
Mach 6.1 (7,470 km/h; 4,640 mph; 2.08 km/s)[source]