RDMT-400A

Engine · Russia

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

NII Mash N2O4/UDMH rocket engine. Developed 1980's. Experimental low-thrust thruster. Niobium combustion chamber with coating.

Engine: 2.80 kg (6.10 lb). Thrust to Weight Ratio: 14.64.

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