Pseudo-boiling and heat transfer deterioration while heating supercritical liquid rocket engine propellants

Heating of liquid propellants used as the coolant in rocket engines may lead to undesired phenomena such as pseudo-boiling or heat transfer deterioration under specific conditions. This can be an issue for propellants characterized at the same time by relatively low critical pressure and temperature. Light hydrocarbons, as for instance methane, belong to this family. In the present paper, a critical review is made of the main results obtained by Authors and their coworkers for the present application. Focus is on the correlations and trends inferred by their numerical simulations mainly carried out considering methane as the coolant, perhaps the most challenging one. (C) 2020 Elsevier B.V. All rights reserved.

Automated summary

This paper critically evaluates the undesired phenomena that may occur when heating liquid propellants used as the coolant in rocket engines, focusing on the correlations and trends inferred by numerical simulations considering methane as the coolant, which is perhaps the most challenging one.