SPACE SYSTEMS
The design and development activities for spacecraft, its subsystems and ground segment are realized in the fields of systems engineering, structure, thermal, electric - electronics, attitude & orbit and spacecraft command & control.
Product design and development tasks are carried out in coordination with engineering process assurance, reliability, maintainability, system safety, concurrent engineering and configuration management disciplines. Product integration and verification phase is completed by the activities of manufacturing engineering, material and process technologies, manufacturing, assembly, integration and test groups.
The rules of European Cooperation for Space Standardization (ECSS) defined by European Space Agency (ESA) are basis of the executing activities and development of quality infrastructure.
ENGINEERING
Manufacturing Engineering:
Manufacturing Engineering, which is responsible from the preparation of all technical data that forms the basis of a proposal during development process, is responsible from generation of assembly concept, analyzing manufacturing capabilities, determination of tooling requirements, creation of detail and assembly manufacturing work instructions, and maintaining per changes and requests coming from customer, coordination of design problems with design owner, determination of aircraft function tests in the design and production process of a product.
Engineering Process Assurance, Airworthiness and Certification
• Engineering Process Assurance: Responsible for definition, documentation, implementation and improvement of design and engineering processes, deployment of necessary tools as well as informing and keeping the Design and Engineering organization updated.
• Airworthiness and Certification: Responsible for ensuring that products developed through development and modernization programs comply with the applicable Airworthiness Regulations (CS, FAR etc) and EASA Part 21A.239 (a).
STRUCTURAL DESIGN
Structural Design:
The structural design alternatives are established in the early stages of design and updated throughout the design phase within a concurrent engineering environment taking into consideration the cost, material alternatives, manufacturability, maintainability, supportability and accessibility aspects.
Structural Analysis:
Static, dynamic, aeroelastic, fatigue and damage tolerance analyses are performed to demonstrate the compliance with design and certification requirements.
Systems Engineering:
• Systems Engineering: Responsible for defining customer needs and required functionality early in the development cycle, managing requirements, functional and physical analysis of the product, and product verification.
• Flight/System Safety: Responsible for the management and implementation of the “System Safety Program” to ensure safe flight and landing in the scope of showing compliance to the airworthiness rules defined by Aviation Authorities.
• Reliability: Responsible for identifying reliability targets, ensuring that the developed products fulfill the requirements determined by systems engineering and airworthiness rules within the life cycle and constituting the necessary inputs for system safety discipline.
PRODUCT MANAGEMENT
This is the management that is responsible for A400M components and systems such as Forward Center Fuselage, Emergency Exit Door, Tail Cone, Paratrooper Doors, Rear Ditching Door, Section 17 Upper Shell, Aileron, Spoilers, Lighting and Water&Waste Systems as well as A350 XWB Ailerons, Maaximus, and B787 parts.
Please click for Aerostructure & Satellite Design & Development brochure.
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