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Resin, Polyimide, Laminating High Temperature Resistant, 315 °C (599 °F)
- Aerospace Material Specification
Published November 16, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers a single-component, heat-reactive, thermosetting aromatic system which thermally cures to form a polyimide polymer structure.
This document has been determined to contain basic and stable technology which is not dynamic in nature.
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Data Sets - Support Documents
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|TABLE 1||FLEXURAL STRENGTH AND MODULUS|
|TABLE 2||COMPRESSIVE STRENGTH AND MODULUS|
|TABLE 3||SHORT BEAM SHEAR STRENGTH|
|TABLE 4||CURING CONDITIONS|
|TABLE 5||POSTCURE CONDITIONS|
AMS P Polymeric Materials Committee
Welcome to the AMS-P Polymeric & Composites Materials Committee discussion forum.The AMS-P Polymeric Materials Committee writes and revises Aerospace Material Specifications (AMS), Metric Aerospace Materials Specifications (MAM), Aerospace Recommended Practices (ARP), and Aerospace Information Reports (AIR) for composite material technology as assigned to the committee. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.
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|ASTMD1824||This document is not part of the subscrption.|
|ASTMD1963||This document is not part of the subscrption.|
|ASTMD2344||This document is not part of the subscrption.|
|ASTMD695||This document is not part of the subscrption.|
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