NII 612 kgf (original) (raw)

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NII 612 kgf

Part of RDMT engine series

NII Mash N2O4/UDMH rocket engine. experimental 612.25 kgf / 0.071 metric tons thrust / 0.031tf. Developed. Experimental thruster, 3 thrust levels by 4 valves: 6000 N, 0.7 N, 0.3 N. Specific impulse 326 - 286 sec.

AKA: RDMT-XX. Status: Developed. Thrust: 6.00 kN (1,349 lbf). Specific impulse: 286 s.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: NII Mash. Bibliography: 336.

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