CRP Technology AMC225xe Aluminum Alloy - SiC Composite, T4 Condition

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CRP Technology AMC225xe Aluminum Alloy - SiC Composite, T4 Condition
Categories:	Metal; Metal Matrix Composite; Nonferrous Metal; Aluminum Alloy; 2000 Series Aluminum Alloy
Material Notes:	AMC225xe is a high quality aerospace grade aluminum alloy (AA2124) reinforced with 25% by volume of ultrafine particles of silicon carbide. It is manufactured by a special powder metallurgy route using a proprietary high-energy mixing process which ensures excellent particle distribution and enhances mechanical properties. The key benefits of AMC225xe for structural applications include: weight saving; increased component stiffness; and high fatigue resistance. The combination of properties achieved with AMC225xe provides the potential for outstanding structural performance in a wide range of markets and applications including: Motorsport Performance valve train Cylinder liners Pistons Connecting rods Brake callipers Disk Bells Suspension parts Aerospace & Defense Aero engine vanes Aircraft structure Brakes and Wheels Control Systems Valve Blocks Information provided by CRP Technology.
Vendors:	About CRP Technology CRP Technology (Modena, Italy) develops, manufactures and sells its proprietary high performance composite materials Windform® for professional 3D Printing. It is also distinguished by its know-how in Selective Laser Sintering technology. It offers part production for short- and low-run production, and prototyping services with Windform®. Its specific application fields including but are not limited to: automotive and motorsports, design, aerospace, UAVs, marine, entertainment, defense, and packaging. Click here to view all available suppliers for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
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Physical Properties	Original Value	Comments

Density	2.88 g/cc

Mechanical Properties	Original Value	Comments
Hardness, Vickers	210	HV10
Tensile Strength, Ultimate	65.0 MPa @Temperature 350 °C	short term exposure
	194 MPa @Temperature 260 °C	short term exposure
	530 MPa @Temperature 200 °C	short term exposure
	616 MPa @Temperature 150 °C	short term exposure
	650 MPa @Temperature 20.0 °C
Tensile Strength, Yield	48.0 MPa @Temperature 350 °C	short term exposure
	128 MPa @Temperature 260 °C	short term exposure
	448 MPa @Temperature 200 °C	short term exposure
	474 MPa @Temperature 150 °C	short term exposure
	480 MPa @Temperature 20.0 °C
Elongation at Break	5 %
Modulus of Elasticity	84.0 GPa @Temperature 300 °C
	92.0 GPa @Temperature 250 °C
	102 GPa @Temperature 200 °C
	108 GPa @Temperature 150 °C
	115 GPa @Temperature 20.0 °C
Poissons Ratio	0.30
Fatigue Strength	305 MPa @# of Cycles 1.00e+7	R=-1; Kt=1; Rotating Bend
	340 MPa @# of Cycles 1.00e+6	R=-1; Kt=1; Rotating Bend

Electrical Properties	Original Value	Comments
Electrical Resistivity	0.0000082 ohm-cm

Thermal Properties	Original Value	Comments
CTE, linear	13.4 µm/m-°C @Temperature -75.0 °C
	14.8 µm/m-°C @Temperature -25.0 °C
	16.0 µm/m-°C @Temperature 20.0 °C
	17.6 µm/m-°C @Temperature 75.0 °C
Specific Heat Capacity	0.836 J/g-°C
Thermal Conductivity	150 W/m-K
Melting Point	>= 548 °C	Solidus
Solidus	548 °C

Processing Properties	Original Value	Comments
Processing Temperature	505 °C	Solution Heat Treatment

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.

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NCRPT45 / 130421

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