Engine Model: RDMT-0.8. Designer: NII Mash. Application: Kosmos satellites. Propellants: Nitrogen+Helium. Thrust(vac): 0.80 N (0.17 lbf). Isp: 70 sec. Mass Engine: 0.10 kg (0.22 lb). Chambers: 1. Thrust to Weight Ratio: 0.81. Country: Russia. Status: In Production. Low-thrust cold-gas thruster. Specific impulse 70 / 160 sec.
Bibliography:- Haeseler, Dietrich, Datasheets from NII Mashinostroeniye, Nishnaya Salda,
1992 via Dietrich Haeseler.