
SAE AMS6562
Current
The latest, up-to-date edition.

Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials
Hardcopy , PDF
English
01-08-2023
The purpose of this specification is to allow procurement of defined carbon fiber and fiberglass epoxy prepreg materials corresponding to their statistically derived material properties published in CMH-17 (formerly MIL-HDBK-17).
DocumentType |
Standard
|
Pages |
25
|
PublisherName |
SAE International
|
Status |
Current
|
The purpose of this specification is to allow procurement of defined carbon fiber and fiberglass epoxy prepreg materials corresponding to their statistically derived material properties published in CMH-17 (formerly MIL-HDBK-17). As a result, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall notify the Qualifying Agency per 4.2.1.
SAE AMS6562/1 | Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 35, Class 4, Grade 293, Style 7781 |
ASTM E 1252 : 1998 | Standard Practice for General Techniques for Obtaining Infrared Spectra for Qualitative Analysis |
ASTM D 3776 : 2009 | Standard Test Methods for Mass Per Unit Area (Weight) of Fabric |
ASTM D 2344/D2344M : 2022 | Standard Test Method for Short-Beam Strength of Polymer Matrix Composite Materials and Their Laminates |
ASTM E 290 : 2013 | Standard Test Methods for Bend Testing of Material for Ductility |
ASTM D 3039/D3039M : 2017 | Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials |
ASTM E 168 : 2016 | Standard Practices for General Techniques of Infrared Quantitative Analysis |
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