This article describes an experimental investigation into the flame dynamics of a subscale
rocket combustor operating with five shear-coaxial injectors fed with methane and oxygen …

The objective of this research is to study the impact of main engine parameters on the
performance of a reusable liquid propellant rocket engine (LPRE). For this purpose, after a …

The prediction of wall heat flux at the nozzle throat is of paramount importance in liquid
rocket engine (LRE) design for both sizing and safety purposes. Computational fluid …

Future space exploration missions will require the synergistic integration of potentially
lightweight, high thrust producing, and environmentally sustainable rocket engines. This …

A method for analyzing liquid ligaments of a textural atomization process is presented in this
article for the case of a rocket engine type-assisted atomization process under combustion …

View Video Presentation: https://doi. org/10.2514/6.2022-3275. vid The prediction of wall
heat flux at the nozzle throat is of paramount importance in liquid rocket engine (LRE) …

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 …

The high hot gas temperatures and chamber pressures typical of modern liquid rocket
engines (LREs) yield high local wall heat fluxes which have to be inevitably managed by the …

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 present experimental study, carried out on the Mascotte test bench of ONERA, aims at
characterizing the flame and flow dynamics of a rocket-type combustor equipped with five …