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CYCOM® 5216

Category:	Epoxy , Epoxy; Epoxide
Manufacturer:	Cytec Industries Inc.
Trademark:	CYCOM®
Fillers:	-
Ports:	Qinzhou, Shekou, Shanghai, Ningbo
Delivery Terms	FOB, CIF, DAP, DAT, DDP
PDF:	egoDdL_CYCOM-5216.pdf
PRICE:	Order Products email sales@su-jiao.com

Wechat: WECHAT

Message
CYCOM® 5216 is a 200 - 250°F (93 - 121°C) curing, modified epoxy resin. Service temperature range is -67 to 180°F (-55 to 82°C). This prepreg is manufactured by hot melt processing and is virtually solvent- free. All three fiber materials - carbon, aramid and glass - are available in unidirectional, woven and, on special order, roving forms. Typical applications include rotorblade spars and skins. Carbon fiber reinforced CYCOM 5216 is a good candidate for aircraft secondary structure, commercial aircraft and aerospace products. Aramid reinforced CYCOM 5216 currently has application in helicopter structure, rotorblades and high impact resistant laminates. Glass fiber reinforced CYCOM 5216 is used in military and commercial helicopter blades and structures and is extensively used for engine nacelles.

Message

CYCOM® 5216 is a 200 - 250°F (93 - 121°C) curing, modified epoxy resin. Service temperature range is -67 to 180°F (-55 to 82°C). This prepreg is manufactured by hot melt processing and is virtually solvent- free.

All three fiber materials - carbon, aramid and glass - are available in unidirectional, woven and, on special order, roving forms. Typical applications include rotorblade spars and skins.

Carbon fiber reinforced CYCOM 5216 is a good candidate for aircraft secondary structure, commercial aircraft and aerospace products. Aramid reinforced CYCOM 5216 currently has application in helicopter structure, rotorblades and high impact resistant laminates. Glass fiber reinforced CYCOM 5216 is used in military and commercial helicopter blades and structures and is extensively used for engine nacelles.

General Information
Features	Autoclavable Fatigue Resistant High Flow High Impact Resistance High Strength
Uses	Aerospace Applications Reinforced Panels Structural Parts
Forms	Fabric Fiber Unidirectional Prepreg
Processing Method	Hot Melt

Physical	Nominal Value	Unit
Specific Gravity ¹	1.24	g/cm³

Note Message
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