Angara-1.2
Angara-1.2 during liftoff on its second flight | |
| Function | Small-lift launch vehicle |
|---|---|
| Manufacturer | Khrunichev |
| Country of origin | Russia |
| Size | |
| Height | 42.2 m (138 ft) |
| Diameter | 2.9 m (9 ft 6 in) |
| Mass | ~171.5 t (378,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload to LEO | |
| Altitude | 200 km (120 mi) |
| Mass | 3,500 kg (7,700 lb) |
| Payload to SSO | |
| Mass | 2,400 kg (5,300 lb) |
| Payload to LEO | |
| Altitude | 1,500 km (930 mi) |
| Mass | 1,600 kg (3,500 lb) |
| Associated rockets | |
| Family | Angara |
| Launch history | |
| Status | Active |
| Launch sites | Plesetsk, Site 35 |
| Total launches | 6 |
| Success(es) | 6 |
| First flight | 9 July 2014 |
| Last flight | 25 November 2025 (most recent) |
| First stage – URM-1 | |
| Powered by | 1 × RD-191 |
| Maximum thrust | 1,920 kN (430,000 lbf) |
| Specific impulse | 310.7 s (3.047 km/s) |
| Burn time | 214 seconds |
| Propellant | LOX / RP-1 |
| Second stage – URM-2 | |
| Powered by | 1 × RD-0124A |
| Maximum thrust | 294.3 kN (66,200 lbf) |
| Specific impulse | 359 s (3.52 km/s) |
| Burn time | 424 seconds |
| Propellant | LOX / RP-1 |
Angara-1.2 is a Russian two-stage small-lift launch vehicle designed to launch a payload of up to 3.5 t (7,700 lb) into low Earth orbit and up to 2.4 t (5,300 lb) into a sun-synchronous orbit. The height of the Angara-1.2 is about 41.5 m (136 ft), the launch mass of the rocket is about 171.5 t (378,000 lb). It is part of the Angara family of launch vehicles.