Upgrade UAS platform to new materials
Consolidation of existing global FE models
Modeling of the applicable loads
Static analysis
Stability analysis
Strength check of FRP & metallic structures
Check of primary interfaces
Bonded and fastened joints’ check
Preparation of structural analysis reports for UAS certification

Development of the new empennage FE model.

Sizings, Static structural justification of the empennages and boom.

Thermal analysis (Avionics), Static structural analysis of the UAS body, load application, FEA , Certification Reports

Engineering contractor for the development of a family of UAS
Responsible for the airframes
Responsible for the mechanisms
Design (from preliminary stage to manufacturing drawings)
Optimization w.r.t. manufacturing costs and flight range
Manufacturing support
Certification
Liaisoning with other sub-system level contractors