RM-2005 350oF Cure Toughened Epoxy Prepreg - Renegade ......Renegade Materials RM-2005 is a 350 F...

RM-2005 350oF Cure Toughened Epoxy Prepreg

FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS

3363 South Tech Boulevard Miamisburg, OH 45342 Tel: 937-350-5274 Page 1

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.

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 structural applications.

RM-2005 is readily available with no minimum order quantities and the fastest lead times in the

industry.

Typical RM-XXXX Resin Properties

RM-2005 Resin Properties

Cured Resin Density 1.26 g/cc

Resin Flex Strength 25 ksi

Resin Flex Modulus 526 Msi

Resin Flex Strain to Failure 5.0 %

Straightforward 350°F Cure.

Designed for demanding aerospace structural applications.

Developed for optimized tack and handle ability.

Delivers an excellent balance of properties for service up to 300oF.

Available in woven, unidirectional and slit-tape product forms using all fibers including carbon,

quartz and glass.

Nano-enhancements for tailored laminate properties and multi-functional performance available.



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.)

RM-2005-IM7-12K-GP Unitape

Property Test Method Test Condition Test Result

0o Tensile Strength (ksi) ASTM D 3039 RT Dry 390

0o Tensile Modulus (Msi) ASTM D 3039 RT Dry 23.9

0o Compression Strength (ksi) ASTM D 3410 RT Dry 240

0o Compression Modulus (Msi)

ASTM D 3410 RT Dry 20.9

Flexural Strength (ksi) ASTM D 790 RT Dry 272

Flexural Modulus (Msi) ASTM D 790 RT Dry 20.7

Interlaminar Shear Strength (ksi)



ASTM D 2344 200°F Dry 13.0

In-Plane Shear Strength (ksi) ASTM D 3518 RT Dry 18.4

In-Plane Shear Modulus (Msi) ASTM D 3518 RT Dry 0.6

Open Hole Compression (ksi) SACMA SRM-3 RT Dry 52.0

Open Hole Tensile (ksi) SACMA SRM-5 RT Dry 58.0

-Properties were generated on Hexcel’s IM7-12K-GP fiber.



Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Unidirectional Tape

(All Data Normalized to 57% Fiber Volume Except for Shear Properties.)

RM-2005-HTS45-12K-E23-Unitape (130 gsm)

Property Test Method Test

Condition* Test Result

0o Tensile Strength (ksi) ASTM D 3039

-75oF Dry 281

RT Dry 335

RT Wet 322

250oF Dry 301

250oF Wet 325


-75oF Dry 12.6

RT Dry 14.1

250oF Wet 3.9

0o Tensile Modulus (Msi) ASTM D 3039

-75oF Dry 19.0

RT Dry 19.6

RT Wet 18.9

250oF Dry 18.8

250oF Wet 20.7


-75oF Dry 1.53

RT Dry 1.37

250oF Wet 0.97

0o Compression Strength (ksi) SRM-1R-94

-75oF Dry 226

RT Dry 234

RT Wet 222

250oF Dry 215

250oF Wet 168


SRM-1R-94

-75oF Dry 18.0

RT Dry 17.8

RT Wet 17.6

250oF Dry 20.0

250oF Wet 19.2

In-Plane Shear Strength (ksi) ASTM D 3518

-75oF Dry 18.6

RT Dry 17.8

250oF Wet 11.8

In-Plane Shear Modulus (Msi) ASTM D 3518

-75oF Dry 0.85

RT Dry 0.73

250oF Wet 0.43



Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Unidirectional Tape

(Continued)

(All Data Normalized to 57% 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 were generated on Toho’s HTS45 standard modulus 12K carbon fiber.

RM-2005-HTS45-12K-E23-Unitape (130 gsm)





250oF Wet 7.4

GIC Fracture Toughness (in-lb/in2)


Open Hole Tensile Strength (ksi)

ASTM D 5766 -75oF Dry 47.7

RT Dry 51.9

Open Hole Tensile Modulus (Msi)

ASTM D 5766 -75oF Dry 7.6

RT Dry 7.3

Open Hole Compression Strength (ksi)

ASTM D 6484 RT Dry 50

250oF Wet 38

Open Hole Compression Modulus (Msi)


250oF Wet 6.6

Compression After Impact (ksi)

SRM-2R-94 RT Dry 24.0

Glass Transition Temperature, Tg Onset at G’ (oF)

ASTM E 1640 Dry 396

Wet 320



Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Plain Weave

(All Data Normalized to 54.5% Fiber Volume)

RM-2005-HTS40-3K-E13-PW Fabric (195 gsm)




-75oF Dry 117

RT Dry 127

RT Wet 126

250oF Dry 143

250oF Wet 138


-75oF Dry 111

RT Dry 115

250oF Dry 126

250oF Wet 124


-75oF Dry 9.6

RT Dry 9.4

RT Wet 9.7

250oF Dry 8.9

250oF Wet 9.4


-75oF Dry 9.4

RT Dry 9.1

250oF Dry 10.1

250oF Wet 9.0


-75oF Dry 144

RT Dry 144

RT Wet 117

250oF Dry 125

250oF Wet 74

RT MEK Soak 144

250oF MEK Soak 100


SRM-1R-94

-75oF Dry 9.2

RT Dry 8.9

RT Wet 9.0

250oF Dry 9.0

250oF Wet 9.0

RT MEK Soak 9.1

250oF MEK Soak 9.9



Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Plain Weave

(Continued)

(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.

RM-2005-HTS40-3K-E13-PW Fabric (195 gsm)



In-Plane Shear Strength (ksi) ASTM D 3518

-75oF Dry 19.0

RT Dry 18.5

250oF Wet 10.5

RT MEK Soak 18.0

250oF MEK Soak 13.9

In-Plane Shear Modulus (Msi) ASTM D 3518

-75oF Dry 0.82

RT Dry 0.74

250oF Wet 0.43

RT MEK Soak 0.67

250oF MEK Soak 0.52


ASTM D 2344

RT Dry 12.6

250oF Dry 9.4

250oF Wet 6.0

GIC Fracture Toughness (in-lb/in2)


Open Hole Tensile Strength (ksi)

ASTM D 5766 -75oF Dry 44

RT Dry 46.6

Open Hole Tensile Modulus (Msi)

ASTM D 5766 -75oF Dry 7.0

RT Dry 6.8

Open Hole Compression Strength (ksi)

ASTM D 6484 RT Dry 47

250oF Wet 30

Open Hole Compression Modulus (Msi)


250oF Wet 6.1

Compression After Impact (ksi)

SRM-2R-94 RT Dry 34


ASTM E 1640 Dry 404

Wet 297



Typical Cured Mechanical Properties for RM-2005 / Standard Modulus Carbon Eight-Harness Satin Weave

(Data Normalized to 54.3% Fiber Volume; Except for Shear and Tg Properties)

RM-2005-HTS40-3K-E13-8HS Fabric (370 gsm)

Property Test Method Test Condition Test Result

0o Tensile Strength (ksi) ASTM D 3039 RT Dry 129

250oF Dry 138

0o Tensile Modulus (Msi) ASTM D 3039 RT Dry 9.1

250oF Dry 9.4


RT Dry 129

250oF Dry 103

0o Compression Modulus (ksi) SRM-1R-94

RT Dry 9.1

250oF Dry 9.3


ASTM E 1640

Dry 399

Wet* 311

*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.



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 of RM-2005 Epoxy Carbon

Plain Weave Cured at the Lower, Nominal, and Upper Cure Cycle Temperature Ranges (G’ Rollover).

0

50

100

150

200

250

300

350

400

450

Gla

ss T

ran

siti

on

Tem

per

atu

re

(G' R

ollo

ver,

°F)

340°F Cure

350°F Cure

360°F Cure



RM-2005 Typical Viscosity Profile

Example RDA Curve for RM-2005 Prepreg.



Recommended Bagging Scheme for RM-2005

Recommended Cure Cycle for RM-2005

All temperatures and times are based upon the lagging thermocouple unless otherwise specified.

Step 1. Vacuum hold for 60 minutes at room temperature Step 2. Heat 1 – 10°F/ minute to 350 ± 10°F apply 30 ± 5 psig pressure until temperature reaches 225 ± 5°F Step 3. Apply 85 ± 5 psig autoclave pressure and vent to atmosphere. Step 4 Hold temperature at 350 ± 10°F for 120 +15/ -0 minutes. Step 5. Cool at 1 – 10°F/ min, when temperature is below 150°F release pressure.



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 express written consent of Renegade Materials.

Revision Date: 31-MAR-2016 KOA
http://www.renegadematerials.com/

RM-2005 350oF Cure Toughened Epoxy Prepreg - Renegade ......Renegade Materials RM-2005 is a 350 F...

Documents

Transcript of RM-2005 350oF Cure Toughened Epoxy Prepreg - Renegade ......Renegade Materials RM-2005 is a 350 F...