Work experience

          

• Dates (from – to)		from the 15/03/06 today
• Name and address of employer		Alenia Aeronautica joint-stock company, Viale dell’Aeronautica SNC 80138, I-80138 Pomigliano D’Arco (NA), Italy (from 15/03/06 to the 30/11/06 time contract with Ergon Line joint-stock company; from 6/12/06 today open-ended contract with Quanta joint-stock corporation).
• Type of business or sector		Aeronautical Company
• Occupation or position held		Aeronautical Designer
• Main activities and responsibilities		Program Boeing 787-Structure Design Engineer (Structural Laboratory) – Horizontal Stabilizer Static and Fatigue Test: Test Structures/Horizontal Stabilizer interface focal point ; Test structures design (Section 48 dummy pivot fitting ; dummy lower gimbal Jackscrew; box for casting pads on elevator; main box loading formers; elevator loading whiffle tree; AuxBox loading supports, Center Box Loading supports, loading tip fittings etc.).

• Dates (from – to)		from the 28/07/05 to the 15/03/06
• Name and address of employer		Alenia Aeronautica joint-stock company, Viale dell’Aeronautica SNC 80138, I-80138 Pomigliano D’Arco (NA), Italy (time contract with Ergon Line joint-stock company).
• Type of business or sector		Aeronautical Company
• Occupation or position held		Aeronautical Designer
• Main activities and responsibilities		Program Boeing 787- Section 44 Structure Design Engineer: Section 44 Skin-Stringer ( Tab-Out definition, ISA construction, Stringer MBD, EMAR, Stringer Ply Sequence, Stringer wrap plies, Stringer modellation); Section 44 Frame (design checks).

Education and training

• Degree in		Aerospace Engineering
• Achieved in the		Academic year 2003-2004
• Voting		110/110 with honours
• Name and type of organization providing education and training		University of the studies of Naples “Federico II”
• Thesis title		"Development of analytical and numerical models for the study of the flight in formation of satellites"
• Thesis description		The purpose of the thesis work has been to estimate the accuracy of analytical models in the long term prediction of the relative motion for formation flying satellites. I have analytically derived and studied Hill’s linearized equations of relative motion that, in the past, have been used to analyze relative motion between satellites in neighbor orbits. Although it’s possible to utilize this model for design several formation type, it’s not able to capture the effect of the J2 gravitational perturbation due to the earth non-sphericity (this is the major motion perturbation for satellites in Low Earth Orbits). To minimize fuel consumption and maximize lifetime, I have derived a new set of constant-coefficient, linearized differential equations that are able to capture the effects of the J2 potential. In order to check the fidelity of the models and demonstrate that the last one  is well suited to model satellites relative motion, I have employed a numerical simulator that simulate the  relative motion of formation flying satellites under the realistic J2  effects.

• School-leaving certificate		Scientific
• Achieved in the		Scholastic year 1995-96
• Voting		50/60
• Name and type of organization providing education and training		Secondary school specializing in scientific studies "Elio Vittorini " of Naples, Italy

Personal skills and competences

Mother tongue

ITALIAN

Other languages

		ENGLISH
• Reading skills		EXCELLENT
• Writing skills		EXCELLENT
• Verbal skills		GOOD

Social- Organizational skills and competences.

Good predisposition to the human contacts, flexibility and enthusiasm for own job, sense of duty and reliability. Work groups coordination in university and working within.

Technical skills and competences .

Complete mastery of the softwares: CATIAV5-ENOVIAV5-IVT-Office package Good mastery of the softwares: MathCAD- Matlab-AutoCAD. Excellent abilities of programming in Matlab environment. Brilliant overcoming of CATIAV5 and ENOVIAV5 courses organized by Alenia Aeronautica.

Driving licence(s)

Type B