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Resin, Polyimide, Laminating High Temperature Resistant, 315 °C (599 °F)
- Aerospace Material Specification
Published November 05, 2010 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 revised to remove specific military requirements described in former sections 184.108.40.206, 5.1.5, and 8.3. MIL-STD-2073-1 was also deleted from section 2.3 since it was referenced in section 5.1.5.
|Aerospace Material Specification||Resin, Polyimide, Laminating High Temperature Resistant, 315 °C (599 °F)|
|Aerospace Material Specification||Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 5 - Carbon Fiber Fabrics, Plain Weave, 193 g/m2, and Epoxy Resin|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|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|
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|AMS2825||MATERIAL SAFETY DATA SHEETS|
|AMS3824||Cloth, Glass, Finished for Resin Laminates|
|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.|
|ASTMD790||This document is not part of the subscrption.|
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