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. It is named after Indian Nobel laureate Sir C.V. Raman.
Description
It uses UDMH and NTO hypergolic propellants. 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.
Development and Testing
- On 12 August 2020, Skyroot Aerospace successfully tested the engine for the first time.
References
- "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.
- Skyroot Aerospace: Raman Engine Test Fire, retrieved 2022-01-25
- "With ISRO assistance, India's Skyroot Aerospace aims maiden rocket launch by Dec-2021". WION. Retrieved 2022-01-25.
- Exclusive Details of Skyroot's Raman Engine, retrieved 2022-01-25
- Narasimhan, T. E. (2020-08-12). "Skyroot Aerospace first private company to test upper stage rocket engine". Business Standard India. Retrieved 2022-01-25.
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