UR-500MK-1

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UR-500MK-1

Part of Polyblock UR-500-1P

LOx/Kerosene propellant rocket stage. Empty mass estimated based on overall vehicle mass fraction. Length estimated based on total mass.

Status: Design 1975. Thrust: 1,637.00 kN (368,012 lbf). Gross mass: 137,000 kg (302,000 lb). Unfuelled mass: 9,300 kg (20,500 lb). Specific impulse: 331 s. Burn time: 250 s. Height: 20.00 m (65.00 ft). Diameter: 4.15 m (13.61 ft). Span: 4.15 m (13.61 ft).

Country: Russia. Engines: NK-33. Launch Vehicles: UR-500MK. Propellants: Lox/Kerosene.

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