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RD-192.2
Part of RD-170 Family
Glushko LOx/LCH4 rocket engine. Developed 1996-on. Proposed variant of RD-192. Staged combustion cycle with fuel-rich gas generator. Gimbaling +/- 8 degree in two planes.

Status: Developed 1996-on. Date: 1996-. Thrust: 1,942.00 kN (436,578 lbf). Specific impulse: 354 s. Specific impulse sea level: 325 s. Height: 3.62 m (11.87 ft). Diameter: 1.45 m (4.75 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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