Ship flight-ready structures lighter, safer, and certified the first time.
We help aerospace teams de-risk CDRs, reduce mass/cost, and pass FAA/NASA reviews without rework.
Teams we've supported across air, space and beyond
What We Do Exceptionally Well
Numerical Methods (FEA)
Structural Design Modifications
- Mass/Stiffness Optimization
- Bolted Joints
- Composite Materials
Structural Static Analysis
- Static / Inertia Loading
- Non-Linear Static
Structural Dynamic Analyses
- Modal Survey
- Random Vibration
- Frequency Dependent Analysis
We’ll flag the top 3 failure risks before CDR.
High Risk Areas not Reliable in FEA Models
Stress Concentration influences
- Access holes
- Laminate ply drops
- Dramatic stiffness changes
- Bolted joints
- Vehicle/large structure repairs (NCRs)
- Model validations to test predictions
Get the Stress Hot-Spot Checklist
Bolted joints, ply drops, cutouts—what to verify before test.
Program Documentation Analysis and Test
Program Documentation Analysis and Test
Structural Certification Plans (NASA, ESA or MIL)
- Certification matrix
- Analysis documentation
- Writing test procedure and plan
- Large and small-scale testing support
Assembly and Integration Support
- Assembly Integration and Test Facility Design
- Clean Room Design
Request a Certification Pack Outline
We’ll map docs, analyses, and test steps for your program.