ABallistic missiles
Hyunmoo
Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile
Preparing your view.
ABallistic missiles
Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile

At a glance
Hyunmoolarger figure on 0 of 1
Kh-47M2 Kinzhallarger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
estimated
Single source7.2 m (23 ft 7 in) (estimated)[source]
Configuration
| Specification | Hyunmoo | Kh-47M2 Kinzhal |
|---|---|---|
| Type | Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile[source] | Air-launched ballistic missile[source] |
| Place of origin | South Korea[source] | Russia[source] |
| In service | 1987–present[source] | 2017–present[source] |
| Used by | Republic of Korea Armed Forces[source] | Russian Aerospace Forces |
Wingspan
Single source1.6 m (5 ft 3 in)[source]
estimated
Single source1,200 mm (47 in) (estimated)[source]
Maximum; Maximum speed
Single sourceMaximum; > Mach 4 (
Single source> Mach 4 (3,045 mph ; 4,900 km/h )[source]
Maximum; Maximum speed
Single sourceMaximum; Up to Mach 10 (
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Agency for Defense Development[source] | Believed to be: Votkinsk Plant State Production Association and Tactical Missiles Corporation JSC[source] |
|---|
| Manufacturer | Hanwha (Hyunmoo-2/4/5) LIG Defense & Aerospace (Hyunmoo-3)[source] | KBM[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] | Low yield nuclear warhead (5 to 50 kt ) or conventional HE[source] |
|---|
| Payload capacity | 500 to 8,000 kg (1,100 to 17,600 lb)[source] | — |
|---|
| Propellant | solid fuel[source] | — |
|---|
| Guidance system | command guidance[source] | INS , mid-course update[source] |
|---|
| Launch platform | mobile launchers[source] | MiG-31BM/K Tu-22M3M Su-34 (reportedly) Su‐57 (planned)[source] |
|---|
| Transport | KM1500[source] | — |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Unit cost | — | US$10 million[source] |
|---|
| Engine | — | Solid-propellant rocket motor[source] |
|---|
| Steering system | — | Four cropped delta‐fins[source] |
|---|
| References | — | Janes , CSIS[source] |
|---|
Up to Mach 10 (3,400 m/s; 11,200 ft/s)[source]