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Vulkan Blok V
Part of N1 Block S Family
LOx/LH2 propellant rocket stage. Upper stage design by KB Saturn for manned lunar expedition, large geosynchronous platform launch.

Status: Development ended 1976. Thrust: 411.00 kN (92,396 lbf). Gross mass: 142,000 kg (313,000 lb). Unfuelled mass: 15,000 kg (33,000 lb). Specific impulse: 460 s. Burn time: 1,370 s. Height: 16.50 m (54.10 ft). Diameter: 6.70 m (21.90 ft). Span: 6.70 m (21.90 ft).

Country: Russia. Engines: RD-57M. Launch Vehicles: Vulkan. Propellants: Lox/LH2.



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