Solvay CYCOM® 7701 Epoxy - Quartz Fiber 8 Harness Satin Fabric Composite

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Solvay CYCOM® 7701 Epoxy - Quartz Fiber 8 Harness Satin Fabric Composite
Categories:	Polymer; Thermoset; Epoxy; Epoxy/Glass SMC
Material Notes:	Composite with Quartz 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.
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Mechanical Properties	Original Value	Comments

Tensile Strength	79000 - 81000 psi @Temperature 24.0 °C	0°
Tensile Modulus	25.0 - 26.0 GPa @Temperature 24.0 °C	0°
Compressive Strength	448 - 462 MPa @Temperature 24.0 °C	0°
Compressive Modulus	24000 - 26000 MPa @Temperature 24.0 °C	0°
Shear Strength	3900 - 4100 psi @Thickness 610 mm	Interlaminar

Thermal Properties	Original Value	Comments
Maximum Service Temperature, Air	93.0 °C	dry

Processing Properties	Original Value	Comments
Processing Temperature	250 °F	Cure Temperature
Shelf Life	0.333 Month @Temperature 22.0 °C
	6.00 Month @Temperature -17.8 °C

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PCYTED083b / 233302

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