Design Verification & Qualification Support

Securing First-Time Pass Certainty for High-Stakes Certification.

In aerospace, defense, and mission-critical industrial sectors, the cost of a "failed test" far exceeds the lab fees. It represents lost months in the development cycle and compromised commercial reputation. We provide the specialist engineering required to steer resonance away from excitation envelopes before the hardware reaches the lab.

Aerospace Heritage: RTCA DO-160 & MIL-STD-810

Leveraging a 15-year legacy across 15 different aircraft platforms, we provide the technical accountability needed to navigate complex environmental testing protocols.

  • Resonance Steering: Engineering the stiffness-to-mass ratio to ensure structural natural frequencies do not coincide with engine-order or rotor-order excitation.
  • Qualification Test Plans (QTP): Developing instrumentation strategies and defining acceptance criteria that satisfy both the standard and the auditor.
  • Predictive Correlation: Using FEA to simulate the test environment, identifying "hot-spots" that require local reinforcement before physical prototyping.

De-Risking the Development Cycle

Our "Design-for-Qualification" methodology reduces the risk of expensive redesign loops by integrating dynamics expertise at the earliest stages of the project.

  • Vibration Isolation & Interface Design: Designing the bespoke mounting strategies required to protect sensitive electronics in high-vibration environments.
  • Random Vibration & PSD Analysis: Simulating structural response under stochastic loading to ensure long-term durability in transport or offshore environments.
  • Technical Traceability: Compiling the evidence packs required for internal design reviews and external regulatory sign-off.

Success Story: Helicopter Blade-Pass Qualification

Case Study: Navigating Critical Certification

A mission-critical instrumentation package was failing during initial vibration sweeps. Our analysis identified a severe resonance coupling with the helicopter's primary blade-pass frequency. Through targeted structural modification and interface isolation, we achieved a first-time pass during the formal qualification phase, saving the client an estimated 4 months of redesign delay.

Explore the Evidence Library →