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AVIMID® R

Category:	PI, TS , Thermoset Polyimide
Manufacturer:	Cytec Industries Inc.
Trademark:	AVIMID®
Fillers:	-
Ports:	Qinzhou, Shekou, Shanghai, Ningbo
Delivery Terms	FOB, CIF, DAP, DAT, DDP
PDF:	COG8uR_AVIMID-R.pdf
PRICE:	Order Products email sales@su-jiao.com

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Message
AVIMID® R is a high temperature, 581°F (305°C) Tg, thermoset polyimide resin with good 500°F (260°C) wet and 550°F (288°C) dry service capability. AVIMID R has outstanding thermal oxidative stability, excellent resistance to aircraft fluids and is tough, showing little micro-cracking during severe thermal cycling. AVIMID R was formulated for prepreg autoclave vacuum bag processing but can be successfully compression molded both as a prepreg and in dry forms as neat resin or chopped-fiber molding compound. Unidirectional tape and woven prepreg of AMIMID R will retain tack and drape for 14 days at 70°F (21°C). Standard autoclave or compression molding processes, to a final temperature of 680°F (360°C) will result in full Tg development/cure, with no need for any post-cure treatment. AVIMID R can be solution impregnated on a variety of fibers and fabrics. Suggested Applications: Jet engine components

Message

AVIMID® R is a high temperature, 581°F (305°C) Tg, thermoset polyimide resin with good 500°F (260°C) wet and 550°F (288°C) dry service capability. AVIMID R has outstanding thermal oxidative stability, excellent resistance to aircraft fluids and is tough, showing little micro-cracking during severe thermal cycling.

AVIMID R was formulated for prepreg autoclave vacuum bag processing but can be successfully compression molded both as a prepreg and in dry forms as neat resin or chopped-fiber molding compound. Unidirectional tape and woven prepreg of AMIMID R will retain tack and drape for 14 days at 70°F (21°C).

Standard autoclave or compression molding processes, to a final temperature of 680°F (360°C) will result in full Tg development/cure, with no need for any post-cure treatment. AVIMID R can be solution impregnated on a variety of fibers and fabrics.

Suggested Applications:
Jet engine components

General Information
Features	Autoclavable Good Crack Resistance Good Thermal Aging Resistance Good Toughness Heat Cure High Heat Resistance Oxidation Resistant
Uses	Aerospace Applications Structural Parts
Forms	Fabric Fiber
Processing Method	Compression Molding Vacuum Forming

Mechanical	Nominal Value	Unit
Tensile Modulus ¹	3590	MPa
Tensile Strength ²	117	MPa
Tensile Elongation (Break)	3.3	%

Thermal	Nominal Value	Unit
Glass Transition Temperature
-- ³	305	°C
-- ⁴	487	°C

Note Message
1 .	Neat resin
2 .	Neat resin
3 .	DMA, Dry
4 .	DMA, Wet

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