Propulsion Technology Team 2_Liquid Rocket Engine Basic Design and Performance Evaluation

You will perform liquid methane rocket engine combustor and basic configuration design, as well as performance evaluation. A Master's degree or higher in aerospace, thermal, or fluid engineering is required, and the role is open to entry-level candidates or those with at least 2 years of experience. You must possess thermal/fluid design skills and experience in liquid rocket engine component and basic design.