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11D121
Part of S1
Korolev GOX/Kerosene rocket engine. N-1 stage 1 (block A) roll control engine. Developed 1969-74. Gimbaling +/- 45 degree. Propellants are fed from main engine (NK-15, NK-33) turbopumps. Chamber Pressure: 71.60 bar.

Status: Developed 1969-74. Date: 1969-74. Thrust: 68.65 kN (15,433 lbf). Specific impulse: 313 s. Specific impulse sea level: 273 s.

Country: Russia. Launch Vehicles: N1F. Propellants: GOX/Kerosene. Stages: N1F Block A. Agency: Korolev bureau. Bibliography: 342, 344.
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