Job Description:
This role is a part of the ATF (Aero Thermal Fluids) group based out of the Canoga Park facility.
Successful candidates will:
Have the capability to lead the analysis, design, and optimization of turbomachinery for liquid rocket engine systems. The ideal candidate will possess deep expertise in the design and performance analysis of inducers, impellers, volutes, pumps, turbines, and other associated rotating machinery operating in cryogenic and high temperature environments. This role requires strong understanding of aerodynamics, thermodynamics, hydrodynamics, and bearing and seal systems and their application to high-speed turbomachineryHave a strong understanding of cavitation and NPSH analysis, rotor-stator interaction, tip leakage flows, secondary flow losses, high-temperature turbine cooling techniquesBe Familiar with engine cycles (gas generator, staged combustion, expander, etc.), cryogenic propellants, high...