Medium Temperature, Out-of-Autoclave, Oven-Vaccum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 32, Class 1, Grade 145, Standard Modulus Fiber 2

Scope:

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 fifth detail spec.

Rationale:

Widely distributed and available industry material specifications are required for procurement of composite materials whose allowables data is published in CMH-17.

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