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Rocket Engine Thermal Analysis Engineer(m/w/x)
Designing cooling concepts and analyzing heat transfer in combustion chambers for reusable space launch systems. Minimum 2 years experience and profound cooling channel design understanding essential. Focus on revolutionary reusable space launch and hypersonic transport systems.
Requirements
- Degree in Space Engineering, Aerospace Engineering, or similar
- Minimum of 2 years of full-time experience
- Strong background in thermal conditions inside rocket engines
- Profound understanding of fluid dynamics, thermodynamics, heat conduction, heat transfer, and radiation
- Profound understanding of cooling channel design
- Proactive thinking, high level of motivation, flexibility, and teamwork skills
- Proficiency in both German and English
Tasks
- Perform thermal design and analysis of rocket engines
- Set up 0D/1D simulations for steady state and transient conditions
- Determine thermal loads from hot gas in the combustion chamber
- Design and assess cooling concepts like regenerative and film cooling
- Analyze heat transfer in combustion chambers and cooling structures
- Define thermal boundary conditions and load cases
- Identify thermal risks and propose design optimizations
- Correlate analytical results with test data for design updates
- Document models, assumptions, results, and design decisions
- Collaborate with design, systems, CFD, test, and manufacturing teams
Work Experience
- 2 years
Education
- Master's degree
Languages
- German – Business Fluent
- English – Business Fluent
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Rocket Engine Thermal Analysis Engineer(m/w/x)
Designing cooling concepts and analyzing heat transfer in combustion chambers for reusable space launch systems. Minimum 2 years experience and profound cooling channel design understanding essential. Focus on revolutionary reusable space launch and hypersonic transport systems.
Requirements
- Degree in Space Engineering, Aerospace Engineering, or similar
- Minimum of 2 years of full-time experience
- Strong background in thermal conditions inside rocket engines
- Profound understanding of fluid dynamics, thermodynamics, heat conduction, heat transfer, and radiation
- Profound understanding of cooling channel design
- Proactive thinking, high level of motivation, flexibility, and teamwork skills
- Proficiency in both German and English
Tasks
- Perform thermal design and analysis of rocket engines
- Set up 0D/1D simulations for steady state and transient conditions
- Determine thermal loads from hot gas in the combustion chamber
- Design and assess cooling concepts like regenerative and film cooling
- Analyze heat transfer in combustion chambers and cooling structures
- Define thermal boundary conditions and load cases
- Identify thermal risks and propose design optimizations
- Correlate analytical results with test data for design updates
- Document models, assumptions, results, and design decisions
- Collaborate with design, systems, CFD, test, and manufacturing teams
Work Experience
- 2 years
Education
- Master's degree
Languages
- German – Business Fluent
- English – Business Fluent
About the Company
POLARIS Raumflugzeuge GmbH
Industry
Aerospace
Description
The company develops a revolutionary reusable space launch and hypersonic transport system that operates like an aircraft.
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