RD-190

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RD-190

Part of RD-120

Glushko LOx/LCH4 rocket engine. Riksha-0 stage 1. Developed 1996-. The RD-190 consists of 6 RD-169 engines. Each chamber can be gimbaled individually in two planes by +/- 8 degree.

Status: Developed 1996-. Date: 1996-. Thrust: 1,000.00 kN (224,800 lbf). Unfuelled mass: 1,470 kg (3,240 lb). Specific impulse: 351 s. Specific impulse sea level: 309 s. Height: 1.70 m (5.50 ft). Diameter: 2.40 m (7.80 ft).

Chambers: 6. Engine: 1,470 kg (3,240 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 69.36. Oxidizer to Fuel Ratio: 3.4.

Country: Russia. Launch Vehicles: Riksha. Propellants: Lox/LCH4. Agency: Glushko bureau. Bibliography: 325.

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