SAE Standards Works
AMS P17 Composite Materials Committee
P1713AH - Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 36, Class 2, Grade 193, Style 3k-70-PW
Not available for purchase at this time.
Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 36, Class 2, Grade 193, Style 3k-70-PW
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the third detail spec.
Widely distributed and available industry material specifications are required for procurement of composite materials whose allowables data is published in CMH-17.