UR-700-2 (original) (raw)

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UR-700-2

N2O4/UDMH propellant rocket stage. .

Status: Development ended 1968. Thrust: 20,182.00 kN (4,537,094 lbf). Gross mass: 1,072,000 kg (2,363,000 lb). Unfuelled mass: 75,600 kg (166,600 lb). Specific impulse: 322 s. Specific impulse sea level: 301 s. Burn time: 306 s. Height: 34.20 m (112.20 ft). Diameter: 8.30 m (27.20 ft). Span: 8.30 m (27.20 ft).

No Engines: 3.

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

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