RD-863
Engine · Ukraine
Original archive entry. The text, images and links below are kept as they were written.
Yuzhnoye N2O4/UDMH rocket engine. MR-UR-100 / RS-16 (SS-17) stage 1 attitude control engine. Out of Production.
Chambers: 4. Engine: 310 kg (680 lb). Chamber Pressure: 88.60 bar. Thrust to Weight Ratio: 91.06. Oxidizer to Fuel Ratio: 2.15.