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Engine Model: RDMT-5. Designer: NII Mash. Application: MMK. Propellants: Air. Thrust(vac): 5.00 N (1.10 lbf). Isp: 70 sec. Mass Engine: 0.35 kg (0.77 lb). Chambers: 1. Thrust to Weight Ratio: 1.45. Country: Russia. Status: In Production. Low-thrust cold-gas thruster.
Bibliography:- Haeseler, Dietrich, Datasheets from NII Mashinostroeniye, Nishnaya Salda,
1992 via Dietrich Haeseler.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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