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RD-863
Yuzhnoye N2O4/UDMH rocket engine. MR-UR-100 / RS-16 (SS-17) stage 1 attitude control engine. Out of Production.

Status: Out of Production. Date: 1970-73. Thrust: 276.84 kN (62,236 lbf). Unfuelled mass: 310 kg (680 lb). Specific impulse: 301 s. Specific impulse sea level: 259 s. Burn time: 130 s. Height: 1.88 m (6.16 ft). Diameter: 2.08 m (6.82 ft).

Chambers: 4. Engine: 310 kg (680 lb). Chamber Pressure: 88.60 bar. Thrust to Weight Ratio: 91.06. Oxidizer to Fuel Ratio: 2.15.

Family: Storable liquid. Country: Ukraine. Launch Vehicles: MR-UR-100. Propellants: N2O4/UDMH. Agency: Yuzhnoye. Bibliography: 348.
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