Aircraft Composite Parts

Our comprehensive facilities conform to the industry’s highest quality standards, and we operate the latest tools and methodologies to ensure benchmark service levels and optimal quality, cost and delivery.

Composite Sandwich Panel
(1) Material:- Carbon Unidirectional Prepreg (Oven Cure)- Nomex Honeycomb Core
(2) Size:- Length : 200mm- Width : 200mm- Edge panel Thickness : 2mm- Sandwich Panel Thickness : 12mm
Stacking Sequence : [45/-45/0/90/0/-45/45]s
Weight : 130g
Maximum Failure Load : 58,920 N (Compression)

Composite I-beam
(1) Material: - Dry Carbon Fabric + Epoxy Resin (RTM Process)
(2) Size:- Length : 480mm- Stiffener Width: 28mm- Skin Width: 68mm- Height : 60mm- Thickness : 2.1mm
Stacking Sequence : [45/0/0/45/0]s
Weight : 300g
Maximum Failure Load : 13,000 N (Bending)