Customer
- Korea Aerospace Research Institute
Project Period
- 1st development : 2013.08 ∼ 2014.01(6 pieces 1st)
- 2nd development : 2014.08 ∼ 2015.01(6 pieces 2nd)
- 3rd development : 2015.02 ∼ 2015.11(One piece)
- Korean launcher application project : 2016.10 ∼ in process
Material
- Carbon fiber/Epoxy
Size
- Outer dia – φ2600mm, Width – 50mm, Height – 35mm
(Customer¡¯s need)
Weight Reduction Rate
-
40% lighter than aluminium part
Performance Index
- Bending stiffness test
Process Type
- Preform, Braiding, VaRTM
Characteristic
- One piece part using the continuous braiding system
- Large scaled composite part
- Mold design after thermal analysis
- Secure the pre-post curing reliability through the resin
curing characteristic analysis
- Ensure the quality by the NDT
(Large scaled CMM measuring, C-scan, X-ray)