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Vulkan 0
LOx/Kerosene propellant rocket stage. Original design of Energia strap-ons, for use with Vulkan booster for manned lunar expedition. Ultimately derived from R-56 of 1961.

AKA: Zenit-1. Status: Development ended 1976. Thrust: 7,891.01 kN (1,773,970 lbf). Gross mass: 355,000 kg (782,000 lb). Unfuelled mass: 35,000 kg (77,000 lb). Specific impulse: 336 s. Specific impulse sea level: 309 s. Burn time: 130 s. Height: 39.00 m (127.00 ft). Diameter: 3.90 m (12.70 ft). Span: 3.90 m (12.70 ft).

Country: Ukraine. Engines: RD-170. Launch Vehicles: Vulkan. Propellants: Lox/Kerosene.



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