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pro vyhledávání: '"Sihan Di"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2024 (2024)
The full-flow staged combustion cycle (FFSC) engine is a promising liquid rocket propulsion system owing to its capacity for high specific impulse. The present study introduces an equilibrium model of the FFSC engine, utilizing the Raptor engine as a
Externí odkaz:
https://doaj.org/article/64c06d173f654ec7a371a255d3226083
