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Angara UM
LOx/Kerosene propellant rocket stage. Can be throttled to 95%. Propellant ration 2.6:1, chamber pressure 257 bar.

Status: In development. Thrust: 2,094.70 kN (470,907 lbf). Gross mass: 140,000 kg (300,000 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 338 s. Specific impulse sea level: 310 s. Burn time: 300 s. Height: 25.00 m (82.00 ft). Diameter: 2.90 m (9.50 ft). Span: 2.90 m (9.50 ft).



Country: Russia. Engines: RD-191. Launch Vehicles: Angara 1.1, Angara-1.2PP, Angara 3A, Angara 5A, Naro-1, KSLV-II, KSLV-III. Propellants: Lox/Kerosene.

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