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RLA-1
LOx/Kerosene propellant rocket stage. Empty mass, specific impulses, length estimated by comparison to smaller Zenit successor design.

Status: Design 1974. Thrust: 11,700.00 kN (2,630,200 lbf). Gross mass: 800,000 kg (1,760,000 lb). Unfuelled mass: 45,000 kg (99,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 210 s. Height: 30.00 m (98.00 ft). Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft).



Country: Russia. Engines: RLA-1200. Launch Vehicles: RLA-120, RLA-150, RLA-135. Propellants: Lox/Kerosene.

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