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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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