“…Modern rockets, such as the Raptor engine developed by SpaceX, make use of a full-flow staged combustion cycle and can reach a combustion chamber pressure of around 300 bar. Under such conditions, the injected liquid fuel may experience a transcritical or supercritical state, as a result of which the governing mechanisms during mixing, evaporation, and combustion will also change. , For example, at low pressures, a distinctive vapor–liquid interface always exists, but as pressure increases, the interface broadens and eventually disappears. − At pressures very close to or beyond the critical point of the mixture, the surface tension vanishes, thereby marking the onset of diffusion-dominated supercritical mixing. , The vapor–liquid interfacial dynamics, especially for mixtures relevant to propulsion applications under extreme conditions, which has not been well understood yet, plays an important role in understanding the mixing, phase transition, and combustion processes. ,, …”