Solvay CYCOM® 7701 Epoxy - 8 Harness Satin Fabric Composite

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.

Solvay CYCOM® 7701 Epoxy - 8 Harness Satin Fabric Composite
Categories:	Polymer; Thermoset; Epoxy; Epoxy/Glass SMC
Material Notes:	Composite with E-Glass Fiber Reinforced 8 Harness Satin Fabric. CYCOM® 7701 resin is a 250°F (121°C) curing epoxy resin designed for use in structural laminates and honeycomb core sandwich panels for aircraft exteriors. In the prepreg form it has excellent drape and tack. CYCOM 7701 was created for autoclave fabrication; however, it can also be press molded and vacuum bag cured. The recommended lay-up procedure for CYCOM 7701 epoxy resin is L-3 or L-6. The recommended cure procedure is C-6 or C-7. Features & Benefits: 250°F (121°C) cure 200°F (93°C) dry service temperature Laminate and sandwich panel usage Self-extinguishing and solvent resistant Self-adhesive to honeycomb core Autoclave, press mold or vacuum bag processing Shelf life 6 months at 0°F (-18°C), 10 days at 72°F (22°C) Applications: Structural laminates and honeycomb core sandwich panels for aircraft exteriors. Information provided by Cytec, subsequently acquired by Solvay.
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.
Printer friendly version Download as PDF Download to Excel (requires Excel and Windows) Export data to your CAD/FEA program Add to Folder:

Mechanical Properties	Metric	English	Comments

Tensile Strength	331 - 352 MPa @Temperature 82.0 °C	48000 - 51000 psi @Temperature 180 °F	0°
	407 - 421 MPa @Temperature 24.0 °C	59000 - 61000 psi @Temperature 75.2 °F	0°
	441 - 462 MPa @Temperature -54.0 °C	64000 - 67000 psi @Temperature -65.2 °F	0°
Tensile Modulus	19.0 - 21.0 GPa @Temperature -54.0 °C	2760 - 3050 ksi @Temperature -65.2 °F	0°
	21.0 - 22.0 GPa @Temperature 82.0 °C	3050 - 3190 ksi @Temperature 180 °F	0°
	22.0 - 24.0 GPa @Temperature 24.0 °C	3190 - 3480 ksi @Temperature 75.2 °F	0°
Compressive Strength	317 - 345 MPa @Temperature 82.0 °C	46000 - 50000 psi @Temperature 180 °F	0°
	441 - 476 MPa @Temperature 24.0 °C	64000 - 69000 psi @Temperature 75.2 °F	0°
	462 - 483 MPa @Temperature -54.0 °C	67000 - 70100 psi @Temperature -65.2 °F	0°
Compressive Modulus	24.0 - 26.0 GPa @Temperature 82.0 °C	3480 - 3770 ksi @Temperature 180 °F	0°
	24.0 - 26.0 GPa @Temperature -54.0 °C	3480 - 3770 ksi @Temperature -65.2 °F	0°
	27.0 - 28.0 GPa @Temperature 24.0 °C	3920 - 4060 ksi @Temperature 75.2 °F	0°
Shear Strength	39.3 - 40.7 MPa @Thickness 2080 mm	5700 - 5900 psi @Thickness 82.0 in	Interlaminar
	66.9 - 69.6 MPa @Thickness 610 mm	9700 - 10100 psi @Thickness 24.0 in	Interlaminar

Thermal Properties	Metric	English	Comments
Maximum Service Temperature, Air	93.0 °C	199 °F	dry

Processing Properties	Metric	English	Comments
Processing Temperature	121 °C	250 °F	Cure Temperature
Shelf Life	0.333 Month @Temperature 22.0 °C	0.333 Month @Temperature 71.6 °F
	6.00 Month @Temperature -17.8 °C	6.00 Month @Temperature 0.000 °F

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 view all the property values for this datasheet as they were originally entered into MatWeb.

Users viewing this material also viewed the following:
Solvay CYCOM® 7701 Epoxy - Quartz Fiber 8 Harness Satin Fabric Composite
Solvay CYCOM® 7701 Epoxy - Crowfoot Satin Fabric Composite

PCYTED083a / 233301

	Advertise with MatWeb!
	Data sheets for over 180,000 metals, plastics, ceramics, and composites.
	HOME • SEARCH • TOOLS • SUPPLIERS • FOLDERS • ABOUT US • FAQ • LOG IN

System Message