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Sponge, Fluorosilicone (FVM) Rubber Closed Cell
- Aerospace Material Specification
Published May 08, 2014 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers a fluorosilicone (FVM) rubber sponge in the form of sheet, strip, extrusions, and molded shapes.
This specification is being revised to clarify that compression-deflection testing will be performed at room temperature and -85 °F.
|Aerospace Material Specification||Vulcanized Fiber Sheet|
|Aerospace Material Specification||Solder, Tin-Lead 45Sn - 55Pb|
|Aerospace Material Specification||Silicone Rubber Extreme Low-Temperature Resistant 35 - 45|
Data Sets - Support Documents
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|TABLE 1B||SI UNITS|
|TABLE 2B||SI UNITS|
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Welcome to the AMS-CE Elastomers Committee Discussion Forum.The AMS-CE Elastomers Committee maintains Aerospace Materials Specifications (AMS), Aerospace Recommended Practices (ARP), Aerospace Information Reports (AIR) and Aerospace Standards (AS) on elastomeric materials. AMS-CE, which reports to the Aerospace Materials Division, coordinates and maintains liaison with industry, government and other standardization groups on elastomeric materials. A significant part of this committee is concerned with elastomeric fluid sealing materials, their applications, material development, testing, quality, design parameters and design practices. 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.
|AMS2810||IDENTIFICATION OF NATURAL AND SYNTHETIC RUBBER MATERIALS|
|ASTMD1056||This document is not part of the subscrption.|
|ASTMD471||This document is not part of the subscrption.|
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