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N1-MOK stage
Part of N1 Block A Family
Air/LOx/LH2 propellant rocket stage. Ultimate derivative of N1 Block A: Propellants changed to LH2/LOX, 16 x modified NK-33 engines + 4 Liquid Air Cycle Engine Liquid Air/LH2 boosters. All figures estimated based on tank volume of Block A and delivery of 90,000 kg payload to 400 kg MKBS orb

AKA: N1-MOK. Status: Study 1974. Thrust: 15,600.00 kN (3,507,000 lbf). Gross mass: 1,200,000 kg (2,600,000 lb). Unfuelled mass: 300,000 kg (660,000 lb). Specific impulse: 430 s. Specific impulse sea level: 875 s. Burn time: 410 s. Height: 30.00 m (98.00 ft). Diameter: 10.00 m (32.00 ft). Span: 17.00 m (55.00 ft).

No Engines: 16.



Country: Russia. Engines: NK-33 LH2 Mod + 4 x LACE. Launch Vehicles: N1-MOK. Propellants: Air/Lox/LH2.

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