RLA-2

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RLA-2

LOx/Kerosene propellant rocket stage. Empty mass, specific impulses, length estimated by comparison to smaller Zenit successor design.

Status: Design 1974. Thrust: 2,940.00 kN (660,930 lbf). Gross mass: 150,000 kg (330,000 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 349 s. Burn time: 160 s. Height: 12.00 m (39.00 ft). Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft).

Country: Russia. Engines: RLA-300. Launch Vehicles: RLA-120, RLA-150, RLA-135. Propellants: Lox/Kerosene.

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