Candidate will work in the ATF (Aero Thermal Fluids) group based out of the Canoga Park facility. The candidate: Shall 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 turbomachinery Shall have a strong understanding of cavitation and NPSH analysis, rotor-stator interaction, tip leakage flows, secondary flow losses, high-temperature turbine cooling techniques Familiarity with engine cycles (gas generator, staged combustion, expander, etc.), cryogenic propellants, high-speed rotating equipment reliability May coordinate risk and opportunity management for development and production programs
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Job Type
Full-time
Career Level
Mid Level