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RD-69M
Yuzhnoye N2O4/UDMH rocket engine. R-36 stage 2 attitude control engine. Out of Production. 4 nozzles, maximum 50 degree gimbal angle.

AKA: D-69M. Status: Out of Production. Date: 1962-1966. Thrust: 54.30 kN (12,207 lbf). Unfuelled mass: 120 kg (260 lb). Burn time: 163 s. Height: 0.90 m (2.95 ft). Diameter: 3.35 m (10.99 ft).

Chambers: 4. Engine: 120 kg (260 lb).



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

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