Sex Male | Date of birth 26/11/1990 | Nationality Italian
Mission analyst, System engineer, Flight dynamics engineer
05/2017–Present NEXT ingegneria dei sistemi, Rome (Italy)
Ground segment system engineer
Actually i am involved on project and offering activities regarding:
-Flight dynamics and mission control system design and developement for mini/nano satellite systems
-System Requirement identification according to ECSS-E-ST-10-06C standard
-System Architecture definition according to ECSS-E-ST-10C standard
-Functional architecture definition
-External interfaces identification (NOAA, IGS, IERS, CDDIS, NORAD)
-Commercial/Open-source Mission operations/Flight dynamics software Trade-off analysis
-Propagator set-up according to ECSS-E-ST-10-04C Space enviornment standard
-Orbit and attitude data message description according to CCSDS standard (AEM-OEM)
-Cubesat technology analysis
-Cubesat commercial and scientific application identification
-Cubsat sub-systems performances analysis (AOCS, EPS, TT&C- Link and power budget implementation)
-Cubesat launch segment analysis: available launchers and launch providers, Dispensers interface
-Cubesat mission cost analysis assessment
05/2016–10/2016 ALI s.c.a.r.l, Naples (Italy)
During this experience i continued working on the prjoects i was involved during the internship. In particual i have performed System engineering and project management activities as:
-Definition and analysis of the system requirements
-Test bed definition
-WBS definition and WP allocation
-Business plan definition
12/2015–05/2016 Euro.Soft s.r.l, Naples (Italy)
Through the thesis work I carried out the Mass Budget, the Power Budget and the Link Budget of a capsule for a small mission to Mars. The work was part of "Small Mars Satellite" ESA Project (Phase 0-A).
-Satellite sub-system weight and size identification
-ESA policy of margin application
-Tsiolkovsky equation implementation and Propellant mass evaluation
-Final launcher payload capability verification
-Mean solar radiation evaluation during the journey to Mars
-Solar radiation evaluation on the Mars region selected
-Concept of operations definition
-Sub-system energy consumption assesment
-Solar panels and battery sizing
-final power budget verification
-Ground and satellite telecommunications system architecture identification .
-link budget implementation
-Earth-Mars Data rate evaluation for both uplink and downlink
06/2015–11/2015 Universitary Intern, ALI s.c.a.r.l, Naples (Italy)
During this period i have been involved in several projects which provided me to acquire new competencies in in terms of:
-Mission Analysis for satellite interplanetary applications
-Write proposals for ESA mission ( phase 0/A )
-Research for fundings ( HORIZON2020, ESA EMITS )
Beside of this i have increased my knowledge about deployable satellites and their applications
EDUCATION AND TRAINING
11/2016–05/2018 Second university of Rome Tor Vergata, Rome (Italy)
II level Master in "Space technology and science", EQF level 8
Subjects of study: astrophysics, orbital mechanics, cosmology, space missions, space flight dynamics, space instruments, management and marketing strategies, system engineering
Mark: 110/110 Cum Laude
Thesis Topic: Defence/survaillance satellite mission for Earth low-mid latitude regions monitoring
Orbit selection activity (orbital parameters selection according to coverage, revisit time, perturbation minimisation, ground track tollerance and maximum off-nadir angle requirements
Orbit control process assessment (DeltaV budget definition according to: Launcher injection error mitigation, atmospheric drag counter-action, collision avoidance and disposal)
Thesis title "Low-mid inclined orbit selection criteria and control assessment"
09/2014–05/2016 University of Naples Federico II, Naples (Italy)
Master degree in aerospace engineering LM-20, class of master degrees in aerospace engineering and astronautics EQF level 7
Main subjects of study: Combustion, Business Administration, III Mathematical Analysis, Aircraft Aerodynamics, Aerospace Construction, Applied Mechanics, Dynamics and Flight Simulation, Space Systems, Avionics, Space Experiments, Hypersonic Aerodynamics, Fluid-Structure Interaction, Aircraft Maintenance
Thesis Topic: Design of a capsule for the "SMS" program (Small Mars Satellite) whose purpose is to develop a mission to Mars to be launched in 2024 on-board of an ESA launcher that shall land at Mars a small payload for scientific experiments. The thesis was elaborated during an internship at the Italian consortium ALI s.c.a.r.l
Mark: 110/110 Cum Laude
Thesis title "Design of a spacecraft for a small Mars mission"
09/2009–12/2013 University of Naples Federico II, Naples (Italy)
Bachelor degree in Aerospace Engineering L-9, class of degrees in industrial engineering
EQF level 6
Subjects of study: Mathematical Analysis, Algebra And Geometry, Physics, Chemistry, Industrial Technical Drawing, Flight Stability and Manoeuvres, Aerodynamics, Gasdynamics, Theory Of Construction, Space Systems, Information Technology, Aerospace Materials Technology, Reliability And Quality, Catia CAD Drawer, Numerical Methods (Matlab), Aerospace Propulsion.
Thesis topic: Study of a double slot synthetic jet as inverter heat – sink from the informatics to the aerodynamic applications.
09/2004–07/2009 Pontano Institute, Naples (Italy)
Scientific high school diploma EQF level 4
Mother tongue(s): Italian
Foreign language(s): English
Spoken interaction: C1
Spoken production: B2
Levels: A1 and A2: Basic user - B1 and B2: Independent user - C1 and C2: Proficient user
Rapid learning and organisational autonomy, practicality, accuracy and curiosity at the same time allow me a rapid learning and the time and resources organisation.
Resistance to stress and capability to bear high working loads gained through a constant study during the academic years.
Flexibility and motivation in terms of professional growth with enthusiasm to learn.
Organisational / managerial skills
Natural inclination to the work group, capability to manage various demands related to different ages or personalities gained through 12 years of scouting
Technical skills and tools
Good skills in Microsoft Office™ tools (Excel, Word, PowerPoint)
Basic usage of Microsoft VISIO
Basic knowledge of OOP language JAVA (v.8, Netbeans as IDE)
Good skills in Matlab usage
Basic usage of CAD software Catia, FEM Analysis software FEMAP
Basic usage of SysML tool IBM Rhapsody
Basic usage of DOORS
Good skills in NASA Mission analysis tool GMAT
Satellite Tool Kit (STK) level 1 certification
Sport High concentration capability obtained through the exercise of martial arts, in order to increase the psycho-physical balance and a possible self defence. Certified as open water Scuba ( up to 18 mt)
Music Guitarist and singer for 10 years
Driving licence: A, B
"THE SMALL MARS SATELLITE: A EUROPEAN SMALL-SIZE MARS LANDER" 7th International Conference on Systems & Concurrent Engineering for Space Applications, SECESA 2016
E. Fantino, R. Aurigemma, D. de la Torre, P. DellAversana, L.Gramiccia, M. Grassi, C. Molfese, F. Paudice, F. Punzo, R. Savino.
"THE SMALL MARS SATELLITE"
E. Fantino, R. Aurigemma, D. de la Torre, P. DellAversana, L.Gramiccia, M. Grassi, C. Molfese, F. Paudice, F. Punzo, R. Savino
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