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Resin prepreg RM-2005, RM-2008
for aeronauticswoven

resin prepreg
resin prepreg
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Characteristics

Matrix
resin
Other characteristics
for aeronautics, woven

Description

FEATURES: High-Performance Materials for Aircraft Applications, both Primary and Secondary Structure Toughened Prepregs Available 250°F, 300°F and 350°F Cure Systems Low Dielectric Epoxy for Radomes and Antennas RM-2005 Toughened Epoxy for Structural Applications 350°F Cure Toughened Excellent Compression Properties Tg - 365°F Large Database Available RM-2008 Modified Epoxy 250°F Cure Good Balance of Properties General Purpose

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.