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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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