Development of Oxygen Drop-Out Boxes for the EMBRAER E2 aircrafts.

My thesis investigates the structural feasibility of integrating high aspect ratio wings to the existing airframe of the Dassault Falcon 7X with minimum modifications in order to reduce Risk and Cost.

My thesis focuses on the preliminary and detailed design of the wings of the Short Take-Off & Landing (STOL) version of the F-14 HERMES aircraft.F-14 HERMES aircraft : Civil Multi-Purpose Air Freighter which missions are typically humanitarian missions, oversize freight transportation, firefighting. 95 students from 22 different nationalities were involved during the design process. Divided in 3 different teams : Structure, Systems and Avionics, which worked together in order to achieve the best possible design.

Space Mission Euclid : under development by the European Space Agency (ESA). The objective of Euclid is to better understand the geometry of dark energy and dark matter by accurately measuring the acceleration of the universe. To achieve this, the spacecraft will measure the redshift of galaxies at varying distances from Earth and investigate the relationship between distance and redshift.MY MISSIONIn partnership with Fresnel Institute and Marseille Astrophysics Laboratory/LAM, I took part in the development of an image processing tool (estimation algorithm based on the maximum likelihood) aiming to estimate parameters of galatic objects (notably the redshift) from their spectral projections.