Job Description

• Design and develop turbopumps for LOX/RP1 rocket engines
• Perform rotor dynamic, fluid dynamic, thermal, and structural analyses of turbopump components
• Use CFD, FEA, and 0D/1D system modelling tools for performance prediction and optimization
• Work on shaft seals, bearings, and lubrication systems
• Collaborate with cross-functional teams, including propulsion, mechanical, and materials engineers, to integrate turbopump systems into the overall rocket engine design
• Define and verify key performance parameters, such as flow rates, pressures, and efficiency, through simulation and testing
• Close collaboration with analysis, manufacturing, procurement, quality, and suppliers
• Oversee the testing and validation of turbopump components and systems to ensure compliance with aerospace standards

• Degree in Space Engineering, Aerospace Engineering (M.Sc.) or similar
• Minimum of 2 years of full-time experience
• Extensive knowledge in turbomachinery, including pumps, turbines and their integration
• Profound understanding of physics, fluid dynamics, manufacturing processes, rocket engine/propulsion systems
• Deep understanding of cryogenic fluids (e.g., LOX) and materials suitable for high-pressure, high-temperature environments.
• Proficiency with Creo and ANSYS Fluent for design and verification
• Proactive thinking, high level of motivation, flexibility, and team-working skills
• Proficiency in both German and English