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11D53F
Part of NK-9
Kuznetsov LOx/Kerosene rocket engine. N1F 1965 - V. Study 1965. As per N1 improvement study, 1965. Engine thrust increased and stretched propellant tanks resulting in 20% longer burn time.

Status: Study 1965. Date: 1965. Thrust: 612.00 kN (137,583 lbf). Specific impulse: 346 s.

Country: Russia. Launch Vehicles: N-IF 1965. Propellants: Lox/Kerosene. Stages: N1F 1965 - V. Agency: Kuznetsov bureau. Bibliography: 283, 306, 319.
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