Designing, analyzing, and optimizing turbopump components for rocket engines, with a focus on liquid oxygen pumps
Making and documenting well-reasoned consequential decisions in turbomachinery design
Carrying out the mechanical design of cryogenic pump components and assemblies based on specifications and best practices
Supervision of external subcontractors and communication with suppliers
Design of test apparatus, definition of test objectives and analysis of test results
Analytical modeling of geometric, mechanical or fluidic problems and implementing solutions in programs
Requirements
Master's degree or higher in Mechanical Engineering, Aerospace Engineering, or a related and applicable technical discipline. Alternatively, a bachelor's degree with substantial relevant experience
Strong fundamentals in fluid mechanics, thermodynamics and mechanical design
Good understanding of industry standard and emerging manufacturing methods and their respective constraints
Proficient in the use of 3D CAD software and drafting
Experience writing software/scripts in languages like Python
Ability to infer system-level implications of component design choices
Strong ability to work in close collaboration with others
Strong oral and written communication skills
Strong analysis and problem-solving skills
Strong research skills and ability to infer useful information from partial or even contradictory sources
Drive towards excellence coupled with ability to work within time constraints
Proficiency in organization and prioritization of tasks
Fluency in English
Some understanding of problems of machine dynamics, such as rotordynamics
Strong understanding of liquid-propellant rocket engines as a system
Proven experience working with any kind of fast rotating machinery
Hands-on experience developing hardware from concept to working prototypes
Benefits
Relocation assistance is provided for those willing to relocate including visa sponsorship where applicable
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