8D726

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8D726

Part of S1

Korolev LOx/Kerosene rocket engine. GR-1 Stage 3, N-11GR - V. Development based on S1.5400.

Thrust: 66.70 kN (14,995 lbf). Specific impulse: 350 s. Burn time: 380 s.

Propellant Formulation: Lox/T-1.

Country: Russia. Launch Vehicles: GR-1, N111, N11GR. Propellants: Lox/Kerosene. Stages: N-11GR - V, GR-1 Stage 3. Agency: Korolev bureau. Bibliography: 177, 21, 64.

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