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NK-19
Part of NK-9
Kuznetsov LOx/Kerosene rocket engine. N-1 stage 4 (Block G). Development ended 1964. Based on NK-9 engine. Originally developed for the modernized second stage of the R-9 (abandoned). Also to have been used on GR-1 / 8K713 Stage 2. First flight 1969.

AKA: 11D54;NK-9V. Status: Development ended 1964. Date: 1960-72. Number: 4 .

Propellant Formulation: Lox/RG-1.



Country: Russia. Launch Vehicles: N111, N11GR, N1 1964, N11 1963, N1 1962, N-IU, N1, N1F, N1 1969. Propellants: Lox/Kerosene. Stages: N1 Block G, N1 1962 - V, N-111-A, N-11 1963 - V, N-11 Block B, N1 1964 - V, N1U 1965 - V, N-111-Ab. Agency: Kuznetsov bureau. Bibliography: 306, 319.

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