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17D61
Status: Design 1999. Thrust: 2.94 kN (662 lbf). Unfuelled mass: 820 kg (1,800 lb). Specific impulse: 326 s. Burn time: 600 s. Height: 2.56 m (8.39 ft). Diameter: 2.72 m (8.92 ft).
Engine thrusts: 1 x 2943 N + 4 x 110 N + 4 x 52 N + 8 x 5.88 N.
Chambers: 1 + 4 + 4 + 8. Engine: 820 kg (1,800 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: .36. Restarts: 50.
Family: Storable liquid. People: Melnikov. Country: Russia. Launch Vehicles: Soyuz 11A511U / Ikar. Propellants: N2O4/UDMH. Stages: Ikar stage. Bibliography: 345, 346, 69.
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