Unha
| Unha-3 at launch pad in April 2012 | |
| Function | Expendable carrier rocket | 
|---|---|
| Manufacturer | National Aerospace Development Administration | 
| Country of origin | North Korea | 
| Size | |
| Height | 28–30 metres (92–98 ft) | 
| Diameter | 2.4 metres (7 ft 10 in) | 
| Mass | 86,750–91,000 kilograms (191,250–200,620 lb) | 
| Stages | 3 | 
| Capacity | |
| Payload to LEO | |
| Mass | 200 kg (440 lb) (465 x 502 km) | 
| Launch history | |
| Status | Active | 
| Launch sites | Sohae, Tonghae | 
| Total launches | 4 | 
| Success(es) | 2 | 
| Failure(s) | 2 | 
| First flight | 5 April 2009 | 
| First stage | |
| Height | 15 m (49 ft) | 
| Diameter | 2.4 m (7 ft 10 in) | 
| Powered by | 4 Nodong 2-1 | 
| Maximum thrust | 1192.8 kN | 
| Specific impulse | 252 sec | 
| Burn time | 120 seconds | 
| Propellant | N2O4/UDMH | 
| Second stage | |
| Height | 8.8–9.3 m (29–31 ft) | 
| Diameter | 1.5 m (4 ft 11 in) | 
| Powered by | 4 verniers | 
| Maximum thrust | 125 kN | 
| Specific impulse | 255 s | 
| Burn time | 220 seconds | 
| Propellant | N2O4/UDMH | 
| Third stage | |
| Height | 3.7–5.7 m (12–19 ft) | 
| Diameter | 1.2–1.25 m (3 ft 11 in – 4 ft 1 in) | 
| Powered by | 2 verniers | 
| Maximum thrust | 35.4 kN | 
| Specific impulse | 230 sec | 
| Burn time | 245 seconds | 
| Propellant | N2O4/UDMH | 
The Unha (Korean: 은하, 銀河, "Galaxy") is a North Korean expendable carrier rocket, which partially utilizes the same delivery system as the Taepodong-2 orbital launch system.