Simulation Study of the Swirl Spray Atomization of a Bipropellant Thruster under Low Temperature Conditions

Simulation Study of the Swirl Spray Atomization of a Bipropellant Thruster under Low Temperature Conditions

The spray atomization of an injector significantly influences the performance and working life span of a bipropellant thruster of a spacecraft. Deep space exploration requires the thruster to be able to operate reliably at a low temperature range from −40 °C to 0 °C, so the effect of low temperature...

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Bibliographic Details
Main Authors: Haifu Li, Jihong Feng, Xinyue Cao, Zhen Zhang, Hongbo Liang, Yusong Yu
Format: Article
Language:English
Published: MDPI AG 2022-11-01
Series:Energies
Subjects:
thrusters
MMH
low temperature
atomization characteristics
VOF
LES
Online Access:https://www.mdpi.com/1996-1073/15/23/8852

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https://www.mdpi.com/1996-1073/15/23/8852

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