Skip to content

Industry

Aerospace Systems & Embedded Engineering

Systems, integration and verification engineering for qualification-oriented environments where every requirement needs evidence.

Aerospace development asks for the same engineering disciplines as other embedded products, with far stricter expectations for traceability, review and documented evidence. CEVOLARION contributes defined engineering work within the customer's process and approval structure.

Evidence is planned with the requirement

In qualification-oriented development each definition level is matched by verification evidence, and the link between them is kept under change control.

  1. Definition: System requirementsEvidence: System verification results
  2. Definition: Architecture and interfacesEvidence: Integration test records
  3. Definition: Hardware and software requirementsEvidence: Component verification results
  4. Definition: Design and implementationEvidence: Reviews and unit-level checks

Where the engineering work sits

The agreed assignment determines which activities are included and where the responsibility boundary sits.

Systems and requirements

Requirement analysis and review, architecture and functional allocation, and decomposition to hardware and software with interfaces made explicit.

Traceability and evidence

Requirement-to-design and requirement-to-test links, maintained through change, so gaps are visible before a review rather than during it.

Hardware/software integration

Integration planning and execution across hardware, embedded software and supplier components, with controlled configurations and reproducible defect isolation.

Verification and qualification support

Test strategy, specification, execution and result analysis, with support for qualification planning and evidence. Environmental or EMC-related work is scoped against the required expertise and facilities.

Typical starting points

  • A requirement set needs review and decomposition before design work can be planned.

  • Traceability has gaps ahead of a customer or authority-facing review.

  • Hardware and software from different teams must be integrated under configuration control.

Capabilities most often involved

System & Software Integration

Integration planning, configuration and dependency management, with defect isolation across software, hardware and supplier boundaries.

How fit is assessed

Aerospace work is assessed with particular care: the applicable standards, the required competence, access and the approval structure are established before a scope is agreed. Engineering support does not confer organisational certification or approval authority.

Common questions

Does CEVOLARION hold aerospace approvals?

Engineering work is contributed within the customer's own process and approval structure. Applicable requirements and approval roles are established for the assignment, and engineering support does not confer organisational certification or approval authority.

Which parts of aerospace development can you take on?

Typical contributions are requirements and traceability work, hardware/software integration and verification. The exact scope depends on the product, the standards that apply and the competence the assignment requires.

Can you perform environmental or EMC testing?

Environmental and EMC qualification support is considered where the assignment and competence support it. Such work is scoped against the required expertise and the test facilities involved.

Discretion is part of the service.

Customer projects, organisations and technical details are not used as marketing material without permission. Fit is established through the scope, engineering methods, responsibility boundary and direct technical discussion.

Discuss an aerospace engineering scope and its evidence requirements.

Start with the product, standards and interfaces that shape the assignment. We will assess the required competence and responsibility together.

Talk to us