Alexander Polidar, M.Sc.
Alexander Polidar studied Mechanical Engineering at the Technical University of Darmstadt and the KTH Royal Institute of Technology in Stockholm. He specialized in Aerospace engineering and fluid mechanics. During his Master’s thesis, he designed an oxidizer-rich preburner for a staged combustion rocket engine at the company Rocket Factory Augsburg. With his experimental research, he aims to advance the flexibility of liquid-oxygen/methane (LOX-methane) rocket engines.
Research
Focus and Interests
- Porous injection systems for LOX-methane rocket engines
- Atomization and flame anchoring
- Optical diagnostics
Projects:
Publications:
Polidar, A., Mair, M., Abplanalp, D., Brieschenk, S. & Manfletti, C. (2022). Design of Open-End Liquid-Liquid Bi-Swirl Coaxial Injectors for Transcritical Injection in an Oxidizer-Rich Preburner. Space Propulsion 2022, Estoril, Portugal.
Polidar & Manfletti, C. (2024). Porous Injectors – The Future of Flexible LOX-Methane Rocket Engines? A Research Roadmap. Space Propulsion 2024, Glasgow, Scotland.