RD-0134

Engine · Russia

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

Kosberg LOx/LNG rocket engine. stage 1. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle variant of RD-0139.

Engine: 1,800 kg (3,900 lb). Thrust to Weight Ratio: 115.44.

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