RM-2005 350o F Cure Toughened Epoxy Prepreg
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RM-2005 350oF Cure Toughened Epoxy Prepreg FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS

RM-2005 350oF Cure Toughened Epoxy Prepreg Renegade Materials RM-2005 is a 350°F Curing Toughened Epoxy Prepreg system. In response to widespread aerospace market demand for an alternative to industry-standard toughened epoxies, Renegade Materials has developed the NEXT generation Toughened Epoxy Prepreg, optimized for both hand-lay-up and automated fiber placement (AFP) processing. RM-2005 is supported by an extensive mechanical property database on both carbon tape and fabric. Excellent mechanical performance and damage tolerance makes RM-2005 a superior choice for military or commercial...

Typical Cured Mechanical Properties for RM-2005 / Intermediate Modulus Carbon Uni-Directional Tape (All Normalized to 60% Fiber Volume Except for In-Plane and Short Beam Shear Properties.) -Properties were generated on Hexcel's IM7-12K-GP fiber. Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274 Page 2

Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Unidirectional Tape (All Data Normalized to 57% Fiber Volume Except for Shear Properties.) Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274 Page 3

Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Unidirectional Tape (Continued) (All Data Normalized to 57% Fiber Volume Except for Shear, G,C and Tg Properties) *Wet Conditioning - 160°F with 85% Relative Humidity to Saturation; Avg. Pick-up - 1.2-1.3% By Weight -Properties were generated on Toho's HTS45 standard modulus 12K carbon fiber. Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342...

Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Plain Weave (All Data Normalized to 54.5% Fiber Volume) Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274 Page 5

(Data Normalized to 54.5% Fiber Volume Except for Shear, GiC and Tg Properties) *Wet Conditioning - 160°F with 85% Relative Humidity to Saturation; Avg. Pick-up - 1.2-1.3% By Weight -Properties generated on Toho's HTS40 3K standard modulus carbon fiber. Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274 Page 6

*Wet Conditioning - 160°F with 85% Relative Humidity to Saturation; Avg. Pick-up - 1.2-1.3% By Weight -Properties generated on Toho's HTS40 3K standard modulus carbon fiber. Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274 Page 7

RM-2005 Glass Transition Temperature Data Glass Transition Temperature, Dry and Wet, of the RM-2005 Epoxy on the Three Reinforcements (G’ Rollover). Glass Transition Temperature (G' Rollover, °F) 340°F Cure 350°F Cure 360°F Cure Glass Transition Temperature of RM-2005 Epoxy Carbon Plain Weave Cured at the Lower, Nominal, and Upper Cure Cycle Temperature Ranges (G’ Rollover). Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg,...

RM-2005 Typical Viscosity Profile Example RDA Curve for RM-2005 Prepreg. Seller makes no warranty regarding the accuracy of this information. Buyers should make their own evaluation to determine suitability of any product for their own intended purposes. 3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274

■EquivalentM aterialscan be used in place of anything listed. 1 - The amount of Bleeders plies to use depends on the target resin content. Bleeders and porous PTFE can be placed on both sides of the laminate or just the top. Peel plies can be used instead of porous PTFE and the glass bleeders 2 - Any steel material capable of withstanding cure conditions, 1/8 inch minimum thickness, cut to same dimensions as prepreg stack-up (do not over-hang edges of lamina). 3 - Use any sealant tape capable of withstanding cure conditions making sure to cover with suitable release film so that not to...

Renegade Materials Corporation is a global leader in manufacturing composite materials for aerospace applications. We deliver light-weight, highly-engineered prepregs, adhesives and hybrid composite systems to enable maximum fuel efficiency in commercial and military aircraft structures. For pricing or additional information on Renegade Material’s products, please visit our website at www.renegadematerials.com This document and any pricing provided on this product, are considered proprietary, confidential and competition-sensitive and are not to be disclosed to any third parties without...