Angara A-2

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Angara A-2

Part of R-7 Block I stage series

LOx/Kerosene propellant rocket stage. Two thrust levels. Propellant ration 2.6:1, chamber pressure 162 bar.

Status: In development. Thrust: 294.00 kN (66,093 lbf). Gross mass: 25,200 kg (55,500 lb). Unfuelled mass: 2,355 kg (5,191 lb). Specific impulse: 359 s. Burn time: 300 s. Height: 6.70 m (21.90 ft). Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft).

Country: Russia. Engines: RD-0124. Launch Vehicles: Angara-1.2PP, Angara 3A. Propellants: Lox/Kerosene.

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