The development of rocket engines to equip future launchers requires a better
understanding of the complex physical phenomena that govern their operation. In the case …

In cryogenic liquid rocket engines, the propellants are usually injected into the combustion
chamber by a coaxial injection system. During transient or lowthrust flight regimes, the …

The space market being more and more competitive, reusable launch vehicles are
envisioned as a key technology to significantly decrease the cost of access to space. As it …

Abstract Combustion in Liquid Rocket Engines (LRE) happens in extreme conditions which
imply several multi-physics phenomena. For this reason, numerical simulation is used to …

La concentration des espèces chimiques comme H₂O, CO₂, CO, K, HCl ainsi que les
grandeurs thermodynamiques comme la pression et la température sont des paramètres …