《AGATE Generic Mat Spec CF Uni》.doc

APPENDIX - 2 Material Specification for T700G-12K-31E/#2510 Advanced Composites – 250 °F Cure – Unidirectional Tape Prepreg of Carbon Fiber and Epoxy Resin ABC Aircraft Company Material Specification for T700G-12K-31E/#2510 Advanced Composites – 250 °F Cure – Unidirectional Tape Prepreg of Carbon Fiber and Epoxy Resin Specification No.: ABC-MS-002 Product P707AG-15 Designation: Original Issue: August XX, 200X Revision Issue: Revision Number: NEW Prepared By: __________________________________ Reviewed By: __________________________________ Reviewed By: __________________________________ Approved By: __________________________________ ABC Company proprietary rights are included in the information disclosed herein. Recipients by accepting this document agrees that neither this document nor the information disclosed herein nor any part thereof shall be transferred or disclosed to third party except as specifically authorized in writing by ABC Company. REVISION RECORD Rev Date Description by Reviewed Approved New Original TABLE OF CONTENTS Section Subject Page 1.0 SCOPE ………………………………………………………… 1 2.0 REFERENCES ………………………………………………… 1 3.0 DEFINITIONS ………………………………………………… 3 4.0 MATERIAL REQUIREMENTS ……………………………… 4 4.1 PREPREG REQUIREMENTS ………………………………... 4 4.1.1 Resin ……………………………………………………………. 4 4.1.2 Carbon Fiber …………………………………………………….. 4 4.1.3 Visual Defect Limitations And Dimensional Requirement ……… 4 4.1.4 Materials Not Conforming To The Visible Defect Limitations And Dimensional Requirements ……………………………….…..… 6 4.1.4.1 For 12 inches, 24 inches and 36 inches Prepreg Material ……….. 6 4.1.4.2 For 3 inches and 6 inches Width Prepreg Material ………………. 7 4.1.5 Prepreg Life Requirement ……………………………………… 7 4.1.6 Uncured Prepreg Physical And Chemical Properties …..…….…. 8 4.2 CURED LAMINA PHYSICAL MECHANICAL PROPERTIES…..………………………………………