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RDMT-50

Engine · Russia

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

NII Mash N2O4/UDMH rocket engine. Kosmos satellites. In Production. Low-thrust attitude control thruster.

Engine: 1.00 kg (2.20 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 5.09.

Country
Russia
Propellants
N2O4/UDMH
Agency
NII Mash
Bibliography
336