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Other Designations: RDMT-XX. Designer: NII Mash. Application: experimental 612.25 kgf / 0.071 tf / 0.031tf. Propellants: N2O4/UDMH Thrust(vac): 612 kgf. Thrust(vac): 6.00 kN. Isp: 286 sec. Chambers: 1. Country: Russia. Status: Developed. References: 336 . Comments: Experimental thruster, 3 thrust levels by 4 valves: 6000 N, 0.7 N, 0.3 N. Specific impulse 326 - 286 sec.
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Last update 12 March 2001.
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© Mark Wade, 2001 .