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BBallistic missiles
Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile
Measured figures
Hyunmoo-5
Single source36,000 kilograms (79,000 lb) (Hyunmoo-5)[source]
Configuration
| Specification | DF-26 | Hyunmoo |
|---|---|---|
| Length | 约15.8米 [1][source] | — |
| Diameter | 1.4米[source] | — |
| Type | IRBM ASBM[source] | Surface-to-surface ballistic missile Surface-to-surface cruise missile Submarine-launched ballistic missile[source] |
| Place of origin | China[source] | South Korea[source] |
| In service | 2016[source] |
Maximum; > Mach 4 (
Single sourceMaximum; Maximum speed
Single source> Mach 4 (3,045 mph ; 4,900 km/h )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1987–present[source] |
| Used by | People's Liberation Army Rocket Force[source] | Republic of Korea Armed Forces[source] |
|---|
| Manufacturer | China Aerospace Science and Technology Corporation[source] | Hanwha (Hyunmoo-2/4/5) LIG Defense & Aerospace (Hyunmoo-3)[source] |
|---|
| Warhead | 1,200–1,800 kg thermonuclear weapon Conventional[source] | Conventional[source] |
|---|
| Engine | Solid-fuel rocket[source] | — |
|---|
| Accuracy | 100 m (330 ft) CEP[source] | — |
|---|
| Launch platform | Mobile launcher[source] | mobile launchers[source] |
|---|
| Status | The Dongfeng-26 or DF-26 ( simplified Chinese : 东风-26 ; traditional Chinese : 東風-26 ; lit. 'East Wind-26'; NATO reporting name : CH-SS-18 ) is an intermediate-range ballistic missile of the Dongfeng series deployed by the People's Liberation Army Rocket Force and produced by the China Aerospace Science and Technology Corporation (CASC).[source] | — |
|---|
| Designer | — | Agency for Defense Development[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] |
|---|
| Payload capacity | — | 500 to 8,000 kg (1,100 to 17,600 lb)[source] |
|---|
| Propellant | — | solid fuel[source] |
|---|
| Guidance system | — | command guidance[source] |
|---|
| Transport | — | KM1500[source] |
|---|