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Batch Qualification Procedure for Tensile Strength, Elongation and Specific Gravity of Polytetrafluoroethylene (PTFE) Resins, Virgin, Modified, Pigmented and Filled Compounds Used for Compression Molding
- Aerospace Standard
- AS4720A
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Standard (AS) covers batch qualification procedure for virgin and compounded polytetrafluoroethylene (PTFE) resins used for compression molding. AS9100 requires virgin and modified PTFE as a testing material be representative of production PTFE and/or parts. The testing specified herein is limited to tensile strength, elongation and specific gravity. Any other tests required by the purchaser must be specified separately.
Rationale
Committee AMP-P voted during the Spring 2012 Meeting that this document should be stabilized.
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Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
TABLE 1 | TENSILE TEST |
Issuing Committee
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.Reference
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