This paper is focused on the investigation of the mechanical property of the carbon fabric/BMI composite laminate. The carbon fabric/BMI composite laminate can be one of light-weight structural materials in aerospace engineering for high temperature a...
This paper is focused on the investigation of the mechanical property of the carbon fabric/BMI composite laminate. The carbon fabric/BMI composite laminate can be one of light-weight structural materials in aerospace engineering for high temperature application over 170℃. The composites laminate plates were made through RTM process. To check the validity of the composite material for the application, the mechanical characteristics of composite specimens from as-received and environmentally conditioned plates were investigated. The mechanical tests were performed according to the MIL-HDBK-17 and ASTM standards