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Manufacturer Name: RD-0234-CH. Designer: Kosberg. Developed in: 1996-. Propellants: Lox/LCH4 Thrust(vac): 45,000 kgf. Thrust(vac): 442.00 kN. Isp: 343 sec. Isp (sea level): 310 sec. Mass Engine: 390 kg. Chambers: 1. Chamber Pressure: 176.00 bar. Oxidizer to Fuel Ratio: 3.40. Country: Russia. Status: Developed 1996-. References: 342 . Comments: Proposed variant of RD-0234 engine using LOX-liquid methane instead of N2O4/UDMH as propellants.
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Last update 12 March 2001.
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