NK-9V-11D53

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NK-9V-11D53

Part of NK-9

Kuznetsov LOx/Kerosene rocket engine. N-1 stage 3 (block V). Out of Production. Modification of NK-9 engine for the N-1 lunar rocket. May be identical to NK-21 (stage 3).

AKA: 11D53;NK-21. Status: Out of Production. Thrust: 449.00 kN (100,939 lbf). Specific impulse: 340 s. Specific impulse sea level: 312 s.

Country: Russia. Propellants: Lox/Kerosene. Agency: Kuznetsov bureau.

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