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UR-700-1
N2O4/UDMH propellant rocket stage. Includes propellant tanks which fed stage two engines from liftoff to first stage cutoff.

Status: Development ended 1968. Thrust: 40,364.00 kN (9,074,188 lbf). Gross mass: 3,210,000 kg (7,070,000 lb). Unfuelled mass: 222,100 kg (489,600 lb). Specific impulse: 322 s. Specific impulse sea level: 301 s. Burn time: 151 s. Height: 53.60 m (175.80 ft). Diameter: 17.60 m (57.70 ft). Span: 24.90 m (81.60 ft).

No Engines: 6.



Country: Russia. Engines: RD-270. Launch Vehicles: UR-700. Propellants: N2O4/UDMH.

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