Raman
Country of originIndia
StatusUnder Development
Hypergolic propellant

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.

Description

It uses UDMH and NTO as its propellant which makes it a Hypergolic Engine.[2] Its injector plate is completely 3D printed. This engine will be used in a cluster of 4 in 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

  • On 12 August 2020, Skyroot Aerospace successfully tested the engine for the first time.[5]

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.


This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.