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 | Shaurya (missile) |
|---|---|---|
| Type | Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile[source] | Short-range ballistic missile[source] |
| Place of origin | South Korea[source] | India[source] |
| In service | 1987–present[source] | — |
| Used by | Republic of Korea Armed Forces[source] | Strategic Forces Command[source] |
Diameter
Single source0.74 m (2.4 ft)[source]
Maximum; > Mach 4 (
Single sourceMaximum; Maximum speed
Single source> Mach 4 (3,045 mph ; 4,900 km/h )[source]
Maximum; 2.55 km/s
Single sourceMaximum; Mach 7.5 (
Single sourceWarhead weight
Single source200–1,000 kilograms (440–2,200 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 Dynamics Limited[source] |
|---|
| Produced | 1980s–present[source] | 2011–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] | Conventional and strategic nuclear weapon[source] |
|---|
| Payload capacity | 500 to 8,000 kg (1,100 to 17,600 lb)[source] | — |
|---|
| Propellant | solid fuel[source] | Solid fuel[source] |
|---|
| Guidance system | command guidance[source] | RLG - INS and accelerometer[source] |
|---|
| Launch platform | mobile launchers[source] | Canisterised transporter erector launcher or underground silo[source] |
|---|
| Transport | KM1500[source] | — |
|---|
| Engine | — | Two-stage solid rocket motor[source] |
|---|
| Flight altitude | — | 50 km (31 mi)[source] |
|---|
| Accuracy | — | 20 m to 30 m CEP[source] |
|---|
| Reported operators | — |
|
|---|
Mach 7.5 (9,190 km/h; 5,710 mph; 2.55 km/s)[source]