Radiative heat flux modeling in rocket propulsion - code 2025IR/01

Qualifications and Interview evaluation up to 60 points or the relevance and significance of qualifications, publications (max 5) and scientific and professional curriculum vitae - up to 31 points for the interview Requirement: Good knoledge of Italian language Master’s degree in Aerospace and Astronautical Engineering obtained no more than six years prior to the application date; Experience in: Knowledge of space propulsion systems and related heat transfer issues; Knowledge of codes for solving the radiative transfer equation and ability to modify them; Familiarity with radiative modeling of gases and particles; Experience in numerical simulation Preferred Skills: Ph.D. degree; Post-graduate scholarships; Contracts and appointments awarded by public or private institutions relevant to the research topic