Hwasong-10
| Hwasong-10 | |
|---|---|
Artist rendition of the missile | |
| Type | Intermediate-range ballistic missile |
| Place of origin | North Korea |
| Service history | |
| In service | Successful test on 22 June 2016 |
| Used by | Korean People's Army Strategic Force Iran (possible) |
| Production history | |
| Manufacturer | North Korea |
| Specifications | |
| Length | 12 m (39 ft) |
| Diameter | 1.5 m (4.9 ft) |
| Warhead |
|
| Warhead weight | 500–1,200 kg (1,100–2,600 lb) (estimated) |
| Engine | Liquid-propellant rocket (same or derived from R-27) |
| Propellant | UDMH and N 2O 4 |
Operational range | 2,500–4,000 km (1,600–2,500 mi) (estimated) |
Guidance system | Inertial guidance |
| Accuracy | 1,600 m (5,200 ft) circular error probable |
Launch platform | MAZ-based transporter erector launcher (TEL) |
| Korean name | |
| Chosŏn'gŭl | 《화성-10》형 |
|---|---|
| Hancha | |
| Revised Romanization | Hwaseong-10 hyeong |
| McCune–Reischauer | Hwasŏng-10 hyŏng |
The Hwasong-10 (Korean: 《화성-10》형; lit. Mars Type 10) is a mobile intermediate-range ballistic missile developed by North Korea.