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Superraket Block A
Part of N1 Block A Family
LOx/Kerosene propellant rocket stage. Ancestor of N1 Block A; conical liquid oxygen/kerosene stage using massive cluster of Kuznetsov engines. Gross mass estimated based on 2,000 metric ton total vehicle weight; empty mass estimated.

Status: Development ended 1959. Thrust: 33,656.00 kN (7,566,169 lbf). Gross mass: 1,150,000 kg (2,530,000 lb). Unfuelled mass: 100,000 kg (220,000 lb). Specific impulse: 310 s. Specific impulse sea level: 270 s. Burn time: 90 s. Height: 27.00 m (88.00 ft). Diameter: 9.00 m (29.50 ft). Span: 15.00 m (49.00 ft).

No Engines: 66.



Country: Russia. Engines: NK-9. Launch Vehicles: Superraket. Propellants: Lox/Kerosene.

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