Engine Model: RDMT-50. Designer: NII Mash. Application: Kosmos satellites. Propellants: N2O4/UDMH. Thrust(vac): 50 N (11 lbf). Isp: 255 sec. Mass Engine: 1.00 kg (2.20 lb). Chambers: 1. Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 5.09. Country: Russia. Status: In Production. Low-thrust attitude control thruster.
Bibliography:- Haeseler, Dietrich, Datasheets from NII Mashinostroeniye, Nishnaya Salda,
1992 via Dietrich Haeseler.