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RD-0242M1
Part of RD-0242
Kosberg N2O4/MMH rocket engine. Design concept 1998-. 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%.

Status: Design concept 1998-. Date: 1998-. Thrust: 98.10 kN (22,054 lbf). Unfuelled mass: 229 kg (504 lb). Specific impulse: 343 s. Burn time: 600 s. Height: 2.34 m (7.67 ft). Diameter: 1.25 m (4.10 ft).

Engine: 229 kg (504 lb). Chamber Pressure: 153.00 bar. Thrust to Weight Ratio: 43.68.

Family: Storable liquid. Country: Russia. Propellants: N2O4/MMH. Agency: Kosberg bureau.
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