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astronautix.com RD-0242M


Manufacturer Name: RD-0242M. Designer: Kosberg. Developed in: 1998-. Propellants: N2O4/MMH Thrust(vac): 10,003 kgf. Thrust(vac): 98.10 kN. Isp: 336 sec. Burn time: 600 sec. Mass Engine: 185 kg. Diameter: 0.8 m. Length: 1.6 m. Chambers: 1. Chamber Pressure: 153.00 bar. Country: Russia. Status: Design concept 1998-. References: 312 . Comments: Proposed variant of RD-0242 engine for upper stages using MMH in place of UDMH (adaptation to western market ?). Reusable for 6 ignitions total. Throttling to 80%. 15 ignitions tested with one single engine.
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Last update 12 March 2001.
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