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
BBallistic missiles
Measured figures
Configuration
| Specification | Hyunmoo | Rampage (missile) |
|---|---|---|
| Type | Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile[source] | — |
| Place of origin | South Korea[source] | Israel[source] |
| In service | 1987–present[source] | — |
| Used by | Republic of Korea Armed Forces[source] | Israeli Air Force Indian Air Force Indian Navy[source] |
| Designer | Agency for Defense Development |
Diameter
Single source306 mm (1.004 ft)[source]
Warhead weight
Single source150 kg (330 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Elbit Systems , Israel Aerospace Industries[source] |
| Manufacturer | Hanwha (Hyunmoo-2/4/5) LIG Defense & Aerospace (Hyunmoo-3)[source] | תעש מערכות ו אלביט מערכות מפעל מלמ של התעשייה האווירית[source]Named manufacturer organization |
|---|
| 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] | Multi- EFP[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] | INS + Altimeter + GPS + Two-way Datalink[source] |
|---|
| Launch platform | mobile launchers[source] | F-16 , F-15 , F/A-18E/F , Eurofighter Typhoon , IAI Kfir , Sukhoi Su-30MKI , SEPECAT Jaguar , MiG-29K[source] |
|---|
| Transport | KM1500[source] | — |
|---|
| Detonation mechanism | — | Radio proximity fuze , Blast fragmentation[source] |
|---|
| Engine | — | Solid-propellant rocket[source] |
|---|
| Flight altitude | — | 3,000–40,000 ft (910–12,190 m)[source] |
|---|
| Accuracy | — | 10m CEP[source] |
|---|