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RD-167
Part of RD-134 Family
Glushko LOx/LCH4 rocket engine. Upper stage. Design concept 1990's. Proposed upper stage engine, a methane variant of RD-134. Gimbaling +/- 3 degree in two planes. Four chambers with one common turbopump.

Status: Design concept 1990's. Thrust: 353.00 kN (79,357 lbf). Unfuelled mass: 570 kg (1,250 lb). Specific impulse: 379 s. Height: 1.60 m (5.20 ft). Diameter: 2.40 m (7.80 ft).

Status 1996 was project, development estimated for four years. Nozzle expansion ratio is 170/0.05=3400.

Chambers: 4. Engine: 570 kg (1,250 lb). Chamber Pressure: 167.00 bar. Thrust to Weight Ratio: 63.15. Oxidizer to Fuel Ratio: 3.4.



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

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