SkyRoot’s Raman-2 Regeneratively Cooled Engine Successfully Achieves Sustained Full-Duration 400 Seconds Burn

Skyroot Aerospace’s Raman-2 engine, named after Sir C.V. Raman, has achieved significant milestones in its development. This regeneratively cooled engine, manufactured using additive manufacturing techniques, utilises Mono Methyl Hydrazine and Nitrogen Tetroxide as hypergolic propellants.It is designed to generate 820 Newton (Sea Level) and 1,460 Newton (Vacuum) thrust, with a nominal chamber
Skyroot Aerospace’s Raman-2 engine, named after Sir C.V. Raman, has achieved significant milestones in its development. This regeneratively cooled engine, manufactured using additive manufacturing techniques, utilises Mono Methyl Hydrazine and Nitrogen Tetroxide as hypergolic propellants.It is designed to generate 820 Newton (Sea Level) and 1,460 Newton (Vacuum) thrust, with a nominal chamber
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