 The design of the Angara-1.2 launch vehicle | |
| Function | Launch vehicle |
|---|---|
| Manufacturer | Khrunichev |
| Country of origin | Russia |
| Size | |
| Height | 42.2 m (138 ft) |
| Diameter | 2.9 m (9 ft 6 in) |
| Mass | ~171,500 kg (378,100 lb)[1] |
| Stages | 2 |
| Capacity | |
| Payload to LEO 200km | |
| Mass | 3,500 kg (7,700 lb)[1] |
| Payload to SSO | |
| Mass | 2,400 kg (5,300 lb) |
| Payload to LEO 1500km | |
| Mass | 1,600 kg (3,500 lb) |
| Associated rockets | |
| Family | Angara |
| Launch history | |
| Status | Active |
| Launch sites | Plesetsk, Site 35 |
| Total launches | 3 |
| Success(es) | 3 |
| Failure(s) | 0 |
| First flight | 9 July 2014 |
| Last flight | 17 September 2024 |
| First stage – URM-1 | |
| Powered by | 1 RD-191 |
| Maximum thrust | 1,920 kN (430,000 lbf) (Sea level) |
| Specific impulse | 310.7 s (3.047 km/s) (Sea level) |
| Propellant | RP-1/LOX |
| 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) |
| Propellant | RP-1/LOX |
"Angara-1.2" is a Russian two-stage small-lift launch vehicle designed to launch a payload of up to 3.5 tons into low Earth orbit and up to 2.4 tons into a sun—synchronous orbit. The height of the "Angara-1.2" is about 41.5 m, the launch mass of the rocket is about 171 tons. It is part of the Angara family of launch vehicles.
- ^ a b "Ракета-носитель "Ангара-1.2"". Роскосмос (in Russian). Archived from the original on 2022-08-21. Retrieved 2022-08-19.