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RD-68M
Yuzhnoye N2O4/UDMH rocket engine. R-36 stage 1 attitude control engine. Out of Production. 4 nozzles, maximum 42 degree gimbal angle.

AKA: D-68M. Status: Out of Production. Date: 1962-1966. Thrust: 285.00 kN (64,070 lbf). Unfuelled mass: 326 kg (718 lb). Burn time: 125 s. Height: 0.98 m (3.21 ft). Diameter: 3.45 m (11.31 ft).

Chambers: 4. Engine: 326 kg (718 lb).



Family: Storable liquid. Country: Ukraine. Launch Vehicles: R-36 8K67M. Propellants: N2O4/UDMH. Agency: Yuzhnoye.

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