Raman Engine

Last updated
Raman
Country of origin India
StatusUnder Development
Liquid-fuel engine
Propellant N2O4 / UDMH
Performance
Thrust850 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.

Contents

Description

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 low compared to many other rocket engines, but is required for precise orbit adjustments. [3] [4]

Development and Testing

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References

  1. "First Indian start-up firm Skyroot Aerospace to test fire rocket engine 'Raman': All you need to know". Jagranjosh.com. 2020-08-17. Retrieved 2022-01-25.
  2. Skyroot Aerospace: Raman Engine Test Fire , retrieved 2022-01-25
  3. "With ISRO assistance, India's Skyroot Aerospace aims maiden rocket launch by Dec-2021". WION. Retrieved 2022-01-25.
  4. Exclusive Details of Skyroot's Raman Engine , retrieved 2022-01-25
  5. Narasimhan, T. E. (2020-08-12). "Skyroot Aerospace first private company to test upper stage rocket engine". Business Standard India. Retrieved 2022-01-25.