Angara A-2
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Two thrust levels. Propellant ration 2.6:1, chamber pressure 162 bar.
Related
- Country
- Russia
- Engines
- RD-0124
- Launch Vehicles
- Angara-1.2PP, Angara 3A
- Propellants
- Lox/Kerosene