RD-0242M

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RD-0242M

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. Reusable for 6 ignitions total. Throttling to 80%.

Status: Design concept 1998-. Date: 1998-. Thrust: 98.10 kN (22,054 lbf). Unfuelled mass: 185 kg (407 lb). Specific impulse: 336 s. Burn time: 600 s. Height: 1.60 m (5.24 ft). Diameter: 0.80 m (2.62 ft).

Adaptation to western market . 15 ignitions tested with one single engine.

Engine: 185 kg (407 lb). Chamber Pressure: 153.00 bar. Thrust to Weight Ratio: 54.07.

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

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