Michele Marcone Email & Phone Number

Colleferro, Lazio, Italia

• Space Rider mission analysis: performance analysis, 3DOF E2E, reentry windows, fragmentation, survivability and risk analysis• Improved re-entry guidance algorithm (-25% propellant consumption)• LV Flight Safety analysis for the far range: fragmentation, survivability, risk at launch• IOS preliminary analysis: performance, propellant budget, phasing• In charge of the main in-house trajectory optimization tool: management, updates and configuration (6 times faster code achieved)• Preliminary and Final Mission Analysis for VEGA flights and support to ArianeSpace and customers• VEGA-E: performance analysis, sizing trajectories, LV Technical Specifcation, 3DOF model for the main optimization tool• SRM and AVUM General Specification• Design of tools: launcher Visibility Analysis, low thrust orbital manoeuvres, Space Rider re-entry simulator• FORTRAN, DRAMA, ELECTRA, MATLAB, STK, DOORS• Knowledge of launcher systems, guidance and optimization

Colleferro, Lazio, Italia

Torino, Italia

Air-launch-to-orbit system with extraction and stabilization by parachutes. Area of expertise:• Parachute recovery system and design methodology;• Dynamic models and stability analysis;• Air-launch-to-orbit technologies;

Master'S Degree, Aerospace Engineering, 110/110 Cum Laude

Bachelor'S Degree, Aerospace Engineering, 102

Maturità Scientifica, P.N.I., 100