Aerospace

Integrated Fuselage

Payload Cap

Topology optimized ribs satisfy stiffness and modal response requirements

Payload Mounts

Optimized supports satisfy stiffness constraints while minimizing vehicle mass

Multi-Node Fuel Tank

Multi-node tank with centerline bond and helical baffles dampen fuel slosh

Intake

Integrated ducting and engine mounting points simplify propulsion assembly

Exhaust

Optimized gyroid structure supports exhaust duct and facilitates heat rejection

Faster

10x reduction in cycle time

2-5x faster new program development

Better

Higher performing product with functional integration

45x reduction in part count

5% mass reduction vs. carbon fiber

Cheaper

2-3x reduction in variable cost

2x reduction in development cost

Zero upfront capex on design specific tooling