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NK-33 LH2 Mod + 4 x LACE
Part of NK-9 Family
Kuznetsov air augmented rocket engine. N1-MOK. Study 1974. Ultimate derivative of NK-9. Propellants changed to LH2/LOX, 16 x modified NK-33 engines + 4 Liquid Air Cycle Engine Liquid Air/LH2 boosters.

AKA: NK-33 LH2 Mod. Status: Study 1974. Date: 1974. Thrust: 980.70 kN (220,470 lbf). Specific impulse: 430 s. Burn time: 410 s.

All figures estimated based on tank volume of Block A and delivery of 90,000 kg payload to 400 kg MKBS orbit.



Family: Air augmented rocket. Country: Russia. Launch Vehicles: N1-MOK. Propellants: Air/Lox/LH2. Stages: N1-MOK stage. Agency: Kuznetsov bureau.

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