Country of origin | India |
---|---|
Status | Under Development |
Liquid-fuel engine | |
Propellant | N2O4 / UDMH |
Performance | |
Thrust | 850 N (190 lbf) |
Raman Engine is a bipropellant rocket engine manufactured by Skyroot Aerospace that will be used in its Vikram family of rockets. [1] It is named after Indian Nobel laureate Sir C.V. Raman.
It uses UDMH and NTO hypergolic propellants. [2] Its injector plate is completely 3D printed. This engine will be used in a cluster of 4 in the fourth stage of the Vikram 1 rocket, which can produce a thrust of 3.4 kN each producing 850 N of thrust, which is lower than many other rocket engines, but is required for precise orbit adjustments. [3] [4]
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