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R-36-0-1
Part of R-36-1 Family
N2O4/UDMH propellant rocket stage. .

Status: Retired 1971. Thrust: 2,640.00 kN (593,490 lbf). Gross mass: 125,000 kg (275,000 lb). Unfuelled mass: 8,500 kg (18,700 lb). Specific impulse: 301 s. Specific impulse sea level: 269 s. Burn time: 120 s. Height: 18.90 m (62.00 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Cost $ : 6.000 million.



Country: Ukraine. Engines: RD-251. Launch Vehicles: R-36O 8K69, R-36O 8K69M. Propellants: N2O4/UDMH.

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