MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Elmet Technologies

(Viewing data as-entered. Click here to return)
Carbon-Core 10 mm+18 oz WR both sides Composite Panels
Categories: Other Engineering Material

Material Notes: Due to anisotropic properties of honeycombs, MIL handbook 17B does not recommend ASTM C393, or 3 point bend test as a valid indicator of honeycomb cored panel behavior. It is viewed as a possible quality control test but not indicative of the real attributes of the structure. It is generally felt that a better indicator would be the ASTM D 6146-99) (Standard Test Method for Two-dimensional Flexural Properties of Simply Supported Sandwich Composite Plates Subjected to a Distributed Load) or also known as “The Hydramat test”. These tests have produced results that validate the accompanying Strength of Materials Data. The viscoelastic behavior of CarbonCore Plastic Honeycomb will typically permit far greater deflections without structural failures so the Deflection at Load is supplied for comparison but this does not imply a Load to fail.

Information provided by Carbon-Core

Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Thickness 448 mil
 
Mechanical PropertiesOriginal ValueComments
Tensile Modulus 1.95e+6 psiDirection 1
 1.95e+6 psiDirection 3
Flexural Stiffness 4972 psi
 
Descriptive Properties
% of each ply's ultimate strength100Direction 1
 100Direction 3
Deflection Values0.12"at 24" span
 0.27"at 36" span
 0.48"at 48" span
Ply Stress<42000 psiDirection 1
 <42000 psiDirection 3

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
Carbon-Core Carbon Balsa Wood
Hexcel® Fibrelam® 5000 Grade 1 Panels for Aircraft Flooring
APCM DA 4080/4082 Epoxy Pregpreg System
Poly-u-Mac GatorBoard WR-26 Fiberglass Reinforced Foam
Poraver Carrier-panel (0.25-0.5 mm), Sandwich panel, Work plate

PCARBC017 / 190836

Ensinger PEI

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at webmaster@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2024 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.