This content is not included in your SAE MOBILUS subscription, or you are not logged in.
POTTING COMPOUND, EPOXY Bisphenol A-Type Filled, Heat Cure, Machinable
- Aerospace Material Specification
Published October 01, 1981 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers an epoxy resin formulation with fillers such as calcium carbonate, supplied as a two-component system, requiring an oven cure for attainment of maximum properties.
Data Sets - Support Documents
|Unnamed Dataset 1|
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.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.