RE-ENTRY VEHICLES

RESEARCH IN RE-ENTRY VEHICLES

Mach Number vs Axial Distance

LES results for the capsule and the DGB parachute entering the atmosphere at Mach 2 

Research focus on the aerothermodynamic analysis of a re-entry space capsule entering the Martian atmosphere at hypersonic speeds with the aim to support planetary entry system design studies.

Performing fully three dimensional CFD analysis to assess the flow field environment around the vehicle by:

In collaboration Prof. Paolo Teofilatto from "Prof. Michele Dicran Sirinian" Flight Mechanics Laboratory at  School of Aerospace Engineering - La Sapienza