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RD-192S
Part of RD-170 Family
Glushko LOx/LCH4 rocket engine. Developed 1996-on. Proposed variant of RD-192. Staged combustion cycle with oxidizer-rich gas generator. Gimbaling +/- 8 degree in two planes.

Status: Developed 1996-on. Date: 1996-. Thrust: 2,128.00 kN (478,393 lbf). Specific impulse: 372 s. Height: 4.82 m (15.81 ft). Diameter: 2.40 m (7.80 ft).

In 1998 prototype development was estimated to take four years from go-ahead.

Chamber Pressure: 196.00 bar. Oxidizer to Fuel Ratio: 3.5.



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

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