RD-0124M

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

Kosberg LOx/Kerosene rocket engine. Developed 1998-. Proposed single chamber variant of RD-0124. Obviously same turbopumps, but one single chamber.

Engine: 360 kg (790 lb). Chamber Pressure: 161.90 bar. Thrust to Weight Ratio: 83.33.

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