Advanced Combustion test Engineer
Listed on 2026-02-08
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Engineering
Aerospace / Aviation / Avionics, Research Scientist, Mechanical Engineer -
Research/Development
Research Scientist
Overview
Powertech is a center of excellence for propulsion technologies, specializing in the design, engineering, and manufacturing of combustion engines, expendable turbojet engines, and turbofan engines for a wide range of aerospace, defence, and autonomous applications, including fixed- and rotary-wing UAVs and other advanced platforms.
Position Overview
Powertech’s Technology Development Team is seeking an Advanced Combustion Test Engineer I to support the development of next-generation propulsion systems for military applications. This role focuses on low- to high-speed combustion aerodynamics, combining experimental testing and high-fidelity numerical simulation across low to mid Technology Readiness Levels (TRL 1–7).
The successful candidate will play a critical role in advancing early-stage concepts through integrated testing, analysis, and modeling, supporting the maturation of innovative propulsion technologies.
Responsibilities- Design, execute, and analyze combustion and high-speed flow experiments, including low-speed and high-speed regimes
- Conduct advanced CFD simulations for reacting and non-reacting flows, including complex combustion aerodynamics
- Develop and validate numerical models using experimental data
- Support propulsion system development activities from TRL 1 (basic research) through TRL 7 (system prototype demonstration)
- Plan and perform experimental campaigns involving high-speed and compressible flows
- Analyze large datasets from simulations and experiments and generate technical reports and presentations
- Collaborate with multidisciplinary teams including propulsion, aerodynamics, materials, and systems engineering
- Support proposal development, technical reviews, and internal technology roadmaps as needed
- Ensure compliance with safety, security, and quality standards associated with military research programs
- PhD in Aerospace Engineering, Mechanical Engineering, or a related field, with a focus on combustion, propulsion, or fluid dynamics
- 2–5 years of post-graduate experience in combustion research, propulsion development, or high-speed aerodynamics
- Strong experience with complex CFD calculations, including reacting flows and turbulence modeling
- Hands-on experience conducting combustion and high-speed flow experiments
- Solid understanding of low-speed and high-speed combustion aerodynamics
- Proficiency with commercial and/or in-house CFD tools and post-processing techniques
- Ability to work effectively in a research-driven, fast-paced development environment
- Experience with propulsion systems for defense or military applications
- Familiarity with experimental diagnostics (e.g., pressure, temperature, optical diagnostics)
- Experience working in low-TRL technology development environments
- Strong technical writing and presentation skills
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