Unlike metals, which have similar properties in all directions (isotropic), the properties of composites vary, dependent on the orientation of the fibers in each layer.
*This diagram illustrates a "generic" layup. The SKU being viewed may not have the layup schedule shown in this diagram. To view this SKU's particular layup, please check out the "LAYUP ORIENTATION" tab.
Application | General Purpose |
---|---|
Shape | Aero / Streamline |
Materials | Standard Modulus Carbon |
Pattern | 3k 2X2 Twill Weave |
Color | Black |
Finish | Satin |
Inside Diameter | 1.905 |
Outside Diameter | 2.045 |
Major ID | 1.905 |
Major OD | 1.905 |
Minor ID | 0.7528 |
Minor OD | 0.7528 |
Length | 40 |
Length (max continuous) | 40.0 |
Linear Density | 0.214 |
Volumetric Density | 0.055 |
Weight | 0.715 |
Primary Fiber | Hexcel AS4 |
Primary Resin / Hardener | Newport 301 |
Max Operating Temp- (Tg) | 250F to 274F |
All laminate properties and mechanical calculations are based on Classical Lamination Theory and should be used as a reference only. Rock West Composites does not guarantee these properties or calculations.
Avg EX Young's Modulus | 9300000.0 |
---|---|
Avg EY Young's Modulus | 9300000.0 |
GXY Shear Modulus | 600000.0 |
X Tensile Yield Strength | 103000.0 |
X Compressive Yield Strength | 89000.0 |
Y Tensile Yield Strength | 103000.0 |
Y Compressive Yield Strength | 89000.0 |
XY Shear Strength | 10618.0 |
CTEX | 2.00E-06 |
CTEY | 2.00E-06 |
Poisson's Ratio vXY | 0.035 |
Poisson's Ratio vYX | 0.035 |
Ply # | Orientation (degrees) | Location |
---|---|---|
1 | All 0/90 | Inside |
We cannot supply theoretical values for this tube at this time. For specification sheets and other data we can supply please review our Technical Spec page.