Filippo Alessandro Fabozzi Email & Phone Number

Massy, Île-De-France, France

As lead mechanical and thermal expert on Exotrail spacevan™ I have successfully devised and led the execution of an end-to-end workflow from specifications to pre-launch testing and qualification of a new mid-weight space vehicle:► Definition of the thermal and structural architecture of Exotrail's OTVs - Proposed, and designed modular structures meeting technical and commercial requirements► Management of manufacturing: led planning, supply, and assembly of full OTV prototypes► Management of testing and qualification: Defined and led numerical and empirical strategies for testing and qualification, completed qualification exchanges with launch subcontractor

Île-De-France, France

Leading a team of 8 engineers for the following activities► Leading of modelling and non-linear static analysis ► Leading for the evaluation of engine fatigue life and damage tolerance► Leading of sizing activities for tooling and test equipment► Evaluation of technical responses to the client specifications

Île-De-France, France

► Detailed sizing of equipped and integrated tanks under the phases of grounding, take off, flight, reentry and landing ► Sizing for combined thermomechanical loads, pressure loads and quasi-static dynamic loads ► Sizing for buckling stability► Verification of modal and vibration modes specifications► Lead of design optimization

Île-De-France, France

► Tool development to automate post-treatments and collection of FEM dynamic modelling results► Tool development to automate the production of synthesis documentation sheets

Île-De-France, France

► Calculation and sizing of composite covers► Development of automated calculation tools for fasteners

Île-De-France, France

► Development of tools for the preliminary estimation of launcher mass► Development of tools for the design and analytical sizing of launcher components► Interaction with and support to the referent system engineer for optimization and interfacing of the different work groups (aerodynamics, mission analysis, propulsion and costing).► Development, correction and validation of codes and tools for the definition of a new fleet of launchers in pre-project phase via automated toolchains in different workflows

Île-De-France, France

► Definition of sizing procedures for metallic and composite structure► Conception, definition and sizing of heavy payload adapter► Trade-off study to benchmark alternative options of non-conventional multi-payload dispensers. Dynamic analysis for payload comfort study. Definition of characteristics and specifications► Dynamic study to solve the problem of high oscillations of a high centering and inertia payloads ► Definition and sizing of a dispenser for a fleet of satellites

Île-De-France, France

► Weekly management of all concessions and change proposals activities► Evaluation of mechanical specifications of non-conformities for subsystems qualification and acceptance testing in dynamic environment► Validation and approval of test reports of primary structures, secondary structures and equipment

Toulouse Area, France

► Conception of global and detailed FEM Model of the central fuselage segment► Development of FEM calculation post-treatment tools► Static and F&DT (Fatigue & Damage Tolerance) sizing of large openings frames (windows, doors etc.)

Toulouse, Occitanie, France

► Weekly management of the development of interfaces between primary structures and equipment► Support to the calculation of secondary structures

Naples, Campania, Italy

► Design of all the fluidic systems of the KA-2HT (Fuel, Air, Oil et Pneumatic Systems)► Definition of specifications and testing specifications for the fluidic equipment suppliers (lines, pumps, valves, reservoirs etc.)

Naples, Campania, Italy

► Design of all the fluidic systems of the KA-2HT (Fuel, Air, Oil et Pneumatic Systems)► Definition of specifications and testing specifications for the fluidic equipment suppliers (lines, pumps, valves, reservoirs etc.)

Program SELENE (May 2010 - May 2011) - InternProgram Falcon 2000DX (Nov 2007 - Jul 2008) - Intern

Master Of Science (M.Sc), Aerospace Engineering, 110/110 Cum Laude

Activities and Societies: Thesis Title: Numerical Modeling Of Two-Phase Flow In Evaporation-Based Heat Transfer DeviceThesis Summary: It.

Bachelor Of Science (B.Sc.), Aerospace Engineering, 105/110

Activities and Societies: Thesis Title: Safety Analysis Of An Aircraft With Tail EnginesThesis Summary: It is evaluated the disposition.