15NT350HT3K_TDS.pdf

NT-350HT Modified Epoxy Prepreg

Description
The NT-350HT Enduredge Max represents the next generation highly
toughened prepreg resin technology. This novel prepreg product offers
outstanding surface finish and laminate quality using vacuum bag only
processing. Unlimited out-time (no refrigerated storage) with zero change in
process parameters over time. NT-350HT allows the parts builder to efficiently
build large out-of-autoclave structures with near zero voids without
complicated debulking processes or elaborate cure cycles. While NT-350HT
was designed for OOA processing, it is perfectly suitable for in-autoclave
processes as well. NT-350HT is suitable for aerospace secondary and primary
structures, space and satellite structures and Radomes.

Product Features
Excellent Mechanical Properties full mechanicals without post-cure
No Freezer Storage; >12 months out-time at ambient storage conditions (70-80 F)
Excellent Mechanical Properties with Vacuum Bag Only processing
Unique engineered air release channels allow excellent OOA processing
Very thick laminates can be produced without any debulk steps
No changes in laminate processing conditions or rheology over time
Optimized for high quality surface finish

Neat Resin Properties
Density 1.17 g/cc
Dielectric Properties: Dk = 2.78 ; Df = 0.013
Moisture Absorption per ASTM D-5229: Post 2.2%, Standard 2.8%

DRY Tg ONSET F ( C) LOSS MODULUS F ( C) TAN DELTA F ( C)
Post 275 F (135 C) 293 F (145 C) 332 F (167 C)
Standard 207 F(97 C) 244 F (118 C) 305 F (152 C)

WET Tg ONSET F ( C) LOSS MODULUS F ( C) TAN DELTA F ( C)
Post 210 F (99 C) 235 F (113 C) 316 F (158 C)
Standard 201 F(94 C) 226 F (108 C) 293 F (145 C)

Prepreg Properties
DRY Tg ONSET F ( C) LOSS MODULUS F ( C) TAN DELTA F ( C)
Post 297 F (147 C) 322 F (161 C) 336 F (169 C)
Standard 244 F (118 C) 268 F (131 C) 302 F (150 C)

Method: ASTM D7028

ALL DATA VACUUM BAG ONLY

Prepreg Electrical Properties on Fiberglass
PROPERTY (0 ) 7781 6781
Dielectric Constant at 10 GHz (dry) 4.10 4.00
Loss Tangent at 10 GHz (dry) 0.012 0.012
Dielectric Constant at 10 GHz (24 hr water boil) 4.19 4.8
Loss Tangent at 10 GHz (24 hr water boil) 0.016 0.094

Prepreg Mechanical Properties on Fiberglass
PROPERTY (0 ) METHOD 7781
Flexural Strength ASTM D7264 103 ksi (711 MPa)
Flexural Modulus ASTM D7264 2.9 Msi (18.5 GPa)
Short Beam Shear ASTM D2344 9.2 ksi (63.6 MPa)
Tensile Strength ASTM D3039 60.4 ksi (416 MPa)
Tensile Modulus ASTM D3039 3.9 Msi (26.9 GPa)
All properties normalized to 60% fiber volume except ILSS (fiber volume 40-50%)

Prepreg Mechanical Properties on Carbon
PROPERTY (0 ) METHOD CARBON FIBER
Tensile Strength ASTM D3039 121 ksi (836 MPa)
Tensile Modulus ASTM D3039 9.52 Msi (65.4 GPa)
Poisson s Ratio ASTM D3039 0.05
Compressive Strength ASTM D6641 93.7 ksi (648 MPa)
Compressive Modulus ASTM D6641 9.71 Msi( 66.7 GPa)
Flexural Strength ASTM D7264 138 ksi (952 MPa)
Flexural Modulus ASTM D7264 8.8 Msi (56.1 GPa)
Short Beam Shear ASTM D2344 9.1 ksi (62.4 MPa)
Open Hole Compression ASTM D6484 42 ksi*
Data normalized to 60% fiber volume
* OHC 3K 2×2 twill AS4D 0/45 all others on 3K Grafil TR30S 2×2 twill

Prepreg Mechanical Properties in Uni-Directional Fibers
Hexcel IM-7 fiber NT-350 resin system autoclave cured
Normalized to 57% fiber content (except SBS)
PROPERTY METHOD RESULT
Tensile Strength ASTM D3039 355 ksi (2451 MPa)
Tensile Modulus ASTM D3039 21.9 Msi (150.4 GPa)
Compressive Strength ASTM D6641 208.9 ksi (1440 MPa)
Compressive Modulus ASTM D6641 20.4 Msi (140.6 GPa)
Flexural Strength ASTM D7264 170.9 ksi (1178.3 MPa)
Flexural Modulus ASTM D7264 19.9 Msi (137.1 GPa)
Short Beam Shear ASTM D2344 12.4 ksi (85.0 GPa)

Layup option for minimal configuration

Layup option for improve bag side. Use this when bag side has to be
taken into consideration.
Poor results unless vacuum is applied throughout full cure process
including while in oven.
ToolSurface
NEXX Layup (up to 25 plies).
Peelply
Solid Teflon film + holesin pattern no closerthan10cm
apart
SealantTape(allaround)
Breather(the thinnerthe better)
Rubbersealant(allaround)
VacuumBag
ReleaseAgent(Marbocote45Eco type)1
2
3
4
5
6
7
8
ToolSurface
NEXX Layup (up to 25 plies).
Teflon film + smallholes(pattern no lessthan10x10cm)
SealantTape(allaround)
Breather(the thinnerthe better)
Rubbersealant(allaround)
VacuumBag
ReleaseAgent(Marbocote45Eco type)1
2
3
4
5
6
7

Layup process for improved bag side

1
2 3
4
5
6
7
8

Proper cure process will show a small leak through the tack hole on the
Teflon film (4) creating a drop on the breather.

TOOL SIDE BAG SIDE

Poor results unless vacuum is applied throughout full cure process
including while in oven.

NT-350HT Baseline Oven Cure

EPOXY PREPREG, ADHESIVE, AND RESIN GUIDELINES AND HANDLING
PROCEDURES
The following guidelines are provided to our customers to assure that best
practices are used to attain the best results from NEXX Technology s epoxy
products. Keep in mind that these procedures represent best practices for all
composite prepreg and adhesive materials.

FREEZER STORAGE
Freezer storage is not required. It will not damage the product but is
completely unnecessary. The product is designed to be kept on the shop floor
at temperatures below 100 F (37 C) for over a year with no changes in
properties, rheology or processing conditions.

MOISTURE ABSORPTION AND SENSITIVITY
While very resistant to moisture absorption after cure, epoxies can be adversely
affected by moisture uptake prior to cure. Other materials may experience
moisture buildup when they are removed from frozen storage. Fortunately, the
Enduredge prepreg does not require freezer storage. It will always be ready for
immediate use

HANDLING MATERIALS
When handling any prepreg materials, always wear clean, powder-free latex
gloves. This assures that no hand oils are transferred to the prepreg and/or
composite during processing. The presence of oils in the part could lead to
problems in both mechanical and electrical performance of the part. This also
guards against dermatitis that may occur with some users.

USE OF HONEYCOMB AND FOAM CORE MATERIALS
When using nonmetallic honeycomb and foam core materials for sandwich
structures, the materials should always be dried in an oven prior to lay-up to
drive off any moisture that may be in the core. The core should be cooled in the
presence of a desiccant to avoid moisture uptake. Following drying, it is always
best to use the material as soon as possible. Recommended core dry
time/temp: 121 C (250 F) for 3-4 hours.

CONTACT INFORMATION
North America & Asia Pacific
NAsales@nexx-technologies.com
(718) 877-6217
Europe, Middle East & Africa
EUsales@nexx-technologies.com
(718) 877-6217

Nexx-Technologies
c/o Mitsubishi Gas Chemical America, Inc.
655 Third Avenue
19
th
Floor
New York, NY 10017
(212) 687-2810
www.enduredge.com
www.mgc-a.com

The information presented herein is believed to be accurate and reliable but is presented without
guarantee of responsibility on the part of Mitsubishi Gas Chemical Company. It is the responsibility
of the users to comply with all applicable laws and regulations and to provide for a safe
workplace. The users should consider any health or safety hazard, or information contained herein
only as a guide, and should take those precautions which are necessary or prudent to instruct
employees and develop work practice procedures in order to promote a safe work environment.
Further, nothing contained herein shall be taken as an inducement or recommendation to
manufacture or use any of the herein materials or processes in violation of existing or future
patents. Mitsubishi Gas Chemical is not affiliated with any other Mitsubishi Group Company.

15NT350HT12K_TDS.pdf

NT-350HT Modified Epoxy Prepreg

Description
The NT-350HT Enduredge Max represents the next generation highly
toughened prepreg resin technology. This novel prepreg product offers
outstanding surface finish and laminate quality using vacuum bag only
processing. Unlimited out-time (no refrigerated storage) with zero change in
process parameters over time. NT-350HT allows the parts builder to efficiently
build large out-of-autoclave structures with near zero voids without
complicated debulking processes or elaborate cure cycles. While NT-350HT
was designed for OOA processing, it is perfectly suitable for in-autoclave
processes as well. NT-350HT is suitable for aerospace secondary and primary
structures, space and satellite structures and Radomes.

Product Features
Excellent Mechanical Properties full mechanicals without post-cure
No Freezer Storage; >12 months out-time at ambient storage conditions (70-80 F)
Excellent Mechanical Properties with Vacuum Bag Only processing
Unique engineered air release channels allow excellent OOA processing
Very thick laminates can be produced without any debulk steps
No changes in laminate processing conditions or rheology over time
Optimized for high quality surface finish

Neat Resin Properties
Density 1.17 g/cc
Dielectric Properties: Dk = 2.78 ; Df = 0.013
Moisture Absorption per ASTM D-5229: Post 2.2%, Standard 2.8%

DRY Tg ONSET F ( C) LOSS MODULUS F ( C) TAN DELTA F ( C)
Post 275 F (135 C) 293 F (145 C) 332 F (167 C)
Standard 207 F(97 C) 244 F (118 C) 305 F (152 C)

WET Tg ONSET F ( C) LOSS MODULUS F ( C) TAN DELTA F ( C)
Post 210 F (99 C) 235 F (113 C) 316 F (158 C)
Standard 201 F(94 C) 226 F (108 C) 293 F (145 C)

Prepreg Properties
DRY Tg ONSET F ( C) LOSS MODULUS F ( C) TAN DELTA F ( C)
Post 297 F (147 C) 322 F (161 C) 336 F (169 C)
Standard 244 F (118 C) 268 F (131 C) 302 F (150 C)

Method: ASTM D7028

ALL DATA VACUUM BAG ONLY

Prepreg Electrical Properties on Fiberglass
PROPERTY (0 ) 7781 6781
Dielectric Constant at 10 GHz (dry) 4.10 4.00
Loss Tangent at 10 GHz (dry) 0.012 0.012
Dielectric Constant at 10 GHz (24 hr water boil) 4.19 4.8
Loss Tangent at 10 GHz (24 hr water boil) 0.016 0.094

Prepreg Mechanical Properties on Fiberglass
PROPERTY (0 ) METHOD 7781
Flexural Strength ASTM D7264 103 ksi (711 MPa)
Flexural Modulus ASTM D7264 2.9 Msi (18.5 GPa)
Short Beam Shear ASTM D2344 9.2 ksi (63.6 MPa)
Tensile Strength ASTM D3039 60.4 ksi (416 MPa)
Tensile Modulus ASTM D3039 3.9 Msi (26.9 GPa)
All properties normalized to 60% fiber volume except ILSS (fiber volume 40-50%)

Prepreg Mechanical Properties on Carbon
PROPERTY (0 ) METHOD CARBON FIBER
Tensile Strength ASTM D3039 121 ksi (836 MPa)
Tensile Modulus ASTM D3039 9.52 Msi (65.4 GPa)
Poisson s Ratio ASTM D3039 0.05
Compressive Strength ASTM D6641 93.7 ksi (648 MPa)
Compressive Modulus ASTM D6641 9.71 Msi( 66.7 GPa)
Flexural Strength ASTM D7264 138 ksi (952 MPa)
Flexural Modulus ASTM D7264 8.8 Msi (56.1 GPa)
Short Beam Shear ASTM D2344 9.1 ksi (62.4 MPa)
Open Hole Compression ASTM D6484 42 ksi*
Data normalized to 60% fiber volume
* OHC 3K 2×2 twill AS4D 0/45 all others on 3K Grafil TR30S 2×2 twill

Prepreg Mechanical Properties in Uni-Directional Fibers
Hexcel IM-7 fiber NT-350 resin system autoclave cured
Normalized to 57% fiber content (except SBS)
PROPERTY METHOD RESULT
Tensile Strength ASTM D3039 355 ksi (2451 MPa)
Tensile Modulus ASTM D3039 21.9 Msi (150.4 GPa)
Compressive Strength ASTM D6641 208.9 ksi (1440 MPa)
Compressive Modulus ASTM D6641 20.4 Msi (140.6 GPa)
Flexural Strength ASTM D7264 170.9 ksi (1178.3 MPa)
Flexural Modulus ASTM D7264 19.9 Msi (137.1 GPa)
Short Beam Shear ASTM D2344 12.4 ksi (85.0 GPa)

Layup option for minimal configuration

Layup option for improve bag side. Use this when bag side has to be
taken into consideration.
Poor results unless vacuum is applied throughout full cure process
including while in oven.
ToolSurface
NEXX Layup (up to 25 plies).
Peelply
Solid Teflon film + holesin pattern no closerthan10cm
apart
SealantTape(allaround)
Breather(the thinnerthe better)
Rubbersealant(allaround)
VacuumBag
ReleaseAgent(Marbocote45Eco type)1
2
3
4
5
6
7
8
ToolSurface
NEXX Layup (up to 25 plies).
Teflon film + smallholes(pattern no lessthan10x10cm)
SealantTape(allaround)
Breather(the thinnerthe better)
Rubbersealant(allaround)
VacuumBag
ReleaseAgent(Marbocote45Eco type)1
2
3
4
5
6
7

Layup process for improved bag side

1
2 3
4
5
6
7
8

Proper cure process will show a small leak through the tack hole on the
Teflon film (4) creating a drop on the breather.

TOOL SIDE BAG SIDE

Poor results unless vacuum is applied throughout full cure process
including while in oven.

NT-350HT Baseline Oven Cure

EPOXY PREPREG, ADHESIVE, AND RESIN GUIDELINES AND HANDLING
PROCEDURES
The following guidelines are provided to our customers to assure that best
practices are used to attain the best results from NEXX Technology s epoxy
products. Keep in mind that these procedures represent best practices for all
composite prepreg and adhesive materials.

FREEZER STORAGE
Freezer storage is not required. It will not damage the product but is
completely unnecessary. The product is designed to be kept on the shop floor
at temperatures below 100 F (37 C) for over a year with no changes in
properties, rheology or processing conditions.

MOISTURE ABSORPTION AND SENSITIVITY
While very resistant to moisture absorption after cure, epoxies can be adversely
affected by moisture uptake prior to cure. Other materials may experience
moisture buildup when they are removed from frozen storage. Fortunately, the
Enduredge prepreg does not require freezer storage. It will always be ready for
immediate use

HANDLING MATERIALS
When handling any prepreg materials, always wear clean, powder-free latex
gloves. This assures that no hand oils are transferred to the prepreg and/or
composite during processing. The presence of oils in the part could lead to
problems in both mechanical and electrical performance of the part. This also
guards against dermatitis that may occur with some users.

USE OF HONEYCOMB AND FOAM CORE MATERIALS
When using nonmetallic honeycomb and foam core materials for sandwich
structures, the materials should always be dried in an oven prior to lay-up to
drive off any moisture that may be in the core. The core should be cooled in the
presence of a desiccant to avoid moisture uptake. Following drying, it is always
best to use the material as soon as possible. Recommended core dry
time/temp: 121 C (250 F) for 3-4 hours.

CONTACT INFORMATION
North America & Asia Pacific
NAsales@nexx-technologies.com
(718) 877-6217
Europe, Middle East & Africa
EUsales@nexx-technologies.com
(718) 877-6217

Nexx-Technologies
c/o Mitsubishi Gas Chemical America, Inc.
655 Third Avenue
19
th
Floor
New York, NY 10017
(212) 687-2810
www.enduredge.com
www.mgc-a.com

The information presented herein is believed to be accurate and reliable but is presented without
guarantee of responsibility on the part of Mitsubishi Gas Chemical Company. It is the responsibility
of the users to comply with all applicable laws and regulations and to provide for a safe
workplace. The users should consider any health or safety hazard, or information contained herein
only as a guide, and should take those precautions which are necessary or prudent to instruct
employees and develop work practice procedures in order to promote a safe work environment.
Further, nothing contained herein shall be taken as an inducement or recommendation to
manufacture or use any of the herein materials or processes in violation of existing or future
patents. Mitsubishi Gas Chemical is not affiliated with any other Mitsubishi Group Company.

15MXB27_TDS.pdf

All information contained in this publication is based upon tests carried out by Colan Products, independent testing authorities or other suppliers.
This information is believed to be correct and reliable at time of printing.
Colan requires that users establish the suitability of all products for their applications and assume all risks.

P R O D U C T D E T A I LS

ITEM CODE: MXB1510DESLT
PRODUCT TYPE: Basalt Stitched Fabric
ORIENTATION: Double Bias +45/-45
INPUT FIBRE:
+45 = Basalt
90 = Basalt
-45 = Basalt
TOTAL WEIGHT: 155 g/m (4.6 oz)
WIDTH: 635 or 1270 mm (25 – 50 )
THICKNESS: 0.25 mm (0.01 )
ROLL LENGTH: 50 metres (54.7 yd)
FINISH: Loomstate

15M7728250_TDS.pdf

HexPly

M77
80 C – 160 C curing epoxy matrix
Product Data Sheet
Description
HexPly

M77 is a formulated epoxy resin matrix, specifically designed for prepreg applications and short cure
cycles. It is a very versatile matrix, allowing a range of processing temperatures from 80 C up to 160 C.
HexPly

M77 is based on a modified epoxy resin. It can be pre-impregnated into carbon, glass or aramid fibers
and exhibits a significant long out-life at room temperature.
Benefits and Features
High toughened epoxy
Excellent tack life
Suitable for a range of pressures (1 to 10 bar)
Short cure cycle at 120 160 C
Good surface finish
Medium tack and excellent drapability
Controlled flow for ease of processing
Long out-life at room temperature
Resin Matrix Properties
T
g
after 130 @15min: 135 C (DSC 25-250 C, 10 C/min)
Density: 1.1 1.2g/cm
Color: Milky
1
Copyright 2016 Hexcel Corporation All Rights Reserved.

Title
Subtitle Product Data Sheet
2
Viscosity
Heating Rate [ C/min] Min. Viscosity * [Pas] Temperature @ * [ C] Time @ * [min]
0.5 15 85 90
2.5 4 100 25
10 3 120 8
25 1.5 135 3
40 10070 130
Complex Viscosity *
1
10
100
1000
10000
100000
1000000
Dyn. 0.5 C/min
40 70 100 130 160
1
100
10
1000
10000
100000
1000000
Dyn. 2.5 C/min
40 10070 130 160 190
1
10
100
1000
10000
100000
1000000
Dyn. 10 C/min
40 70 100 130 160 190
1
100
10
1000
10000
100000
1000000
Dyn. 25 C/min
Temperature [ C]
1
100
10
1000
10000
100000
1000000
Iso 75 C
Iso 85 C
Iso 100 C
Iso 145 C
Complex Viscosity * [Pas]
0 250 500 750 1000 1250 1500 1750 2000 2250 2500 2750 3000
Time [s]
HexPly

M77
80 C – 160 C curing epoxy matrix
Copyright 2016 Hexcel Corporation All Rights Reserved.

Title
Subtitle Product Data Sheet
3
Curing Conditions
The ideal cure cycle is 7 min at 120 C and at a pressure >5bar . Alternative cure cycles can be used:
Temperature Time
110 C 18 min
120 C 7 min
130 C 5 min
140 C 3 min
150 C 2 min
160 C 1.5 min
Prepreg Types and Cured Prepreg Mechanical Properties
Mechanical Properties are based on 130 C cure for 10 min, at 5 bar pressure.
Reinforcement Prepreg data Mechanical data
Fiber
Fabric
Weave
Style
Fabric
Weight
[g/m ]
Fabric
Direction
0 /90
[g/m ]
Weight
[g/m ]
( 5%)
Resin
Content
[%] ( 3)
Tensile
Strength
[MPa]
Tensile
Modulus
[GPa]
ILSS
[MPa]
M77/55%/48P/G Glass plain 47 26/21 104 55 540 28 55
M77/52%/106P/G Glass plain106 54/52 221 52 480 27 67
M77/45%/160P/G Glass plain155 81/74 282 45
M77/38%/395P/G Glass plain386 204/182 623 38
M77/40%/LT570/G+F Glass
non
woven +
fleece
560
432/75
fleece 35
848 35
M77/42%/200T2/CHS-3K Carbon twill200 100/100 345 42
M77/42%/600T2/CHS Carbon twill600 300/3001034 42
M77/38%/UD150/CHS Carbon UD 150 90/0 242 38
M77/39%/UD600/CHS Carbon UD 600 600/0 984 39 2400 140 78
HexPly

M77
80 C – 160 C curing epoxy matrix
Copyright 2016 Hexcel Corporation All Rights Reserved.

Title
Subtitle
2016 Hexcel Corporation All rights reserved. Hexcel Corporation and its subsidiaries ( Hexcel ) believe that the technical data and other information
provided herein was materially accurate as of the date this document was issued. Hexcel reserves the right to update, revise or modify such technical data and
information at any time. Any performance values provided are considered representative but do not and should not constitute a substitute for your own testing of
the suitability of our products for your particular purpose. Hexcel makes no warranty or representation, express or implied, including but not limited to
the implied warranties of merchantability and fitness for a particular purpose, and disclaims any liability arising out of or related to, the use of or
reliance upon any of the technical data or information contained in this document.
For more information
Hexcel is a leading worldwide supplier of composite materials to aerospace and industrial markets.
Our comprehensive range includes:

-or < : Xuotes orders and product infor Tation call toll free 6 4 -or other worldwide sales office telephone numbers and a full address list, please go to: http: www.hexcel.com contact salesoffice HexTow carbon fibers HexForce reinforcements HexPly prepregs HexMC molding compounds HexFlow RTM resins Redux adhesives HexTOOL tooling materials HexWeb honeycombs Acousti-CAP sound attenuating honeycomb Engineered core Engineered products Product Data Sheet 4 Storage and Handling Shelf Life : 18 months Out Life : 6 weeks (42 days) Shelf Life: the maximum storage life for HexPly prepreg, upon receipt by the customer, when stored continuously, in a sealed moisture-proof bag, at -18 C/0 F. To accurately establish the exact expiry date, consult the box label. Out Life: the maximum accumulated time allowed at room temperature between removal from the freezer and cure. Prepreg should be stored as received in a cool dry place or in a refrigerator. After removal from refrigerator storage, prepreg should be allowed to reach room temperature before opening the polyethylene bag, thus preventing condensation. (A full reel in its packing can take up to 48 hours). HexPly M77 80 C - 160 C curing epoxy matrix FTU-296-JA16 HexForce TM 282 Carbon Fabric Style 282 US System Type of Yarns Warp Yarn: 3K Carbon, 33MSI Fill Yarn: 3K Carbon, 33MSI Fabric Weight, Dry 5.70 oz/yd 2 193 g/m 2 Weave Style Plain Construction Nominal Construction Warp Count: 12.5/in 4.92/cm Fill Count: 12.5/in 4.92/cm Fabric Thickness 10. 10 mil 0.26 mm Important All information is believed to be accurate but is given without acceptance of liability. All values have been generated from limited data. The values listed for weight, thickness and breaking strengths are typical greige values, unless otherwise noted. Users should make their own assessment of the suitability of any product for the purpose required. All sales are made subject to our standard terms of sales which include limitations on liability and other important terms. The fabric style listed may not be available from inventory and minimum order quantities may apply. For More Information Hexcel is a leading worldwide supplier of composite materials to aerospace and other demanding industries. Our comprehensive product range includes: Carbon Fiber Reinforced Fabrics Carbon, Glass, Aramid and Hybrid Prepregs RTM Materials HexTOOL composite tooling material Structural Film Adhesives Honeycomb Cores Engineered Core 1913 North King Street Seguin, Texas 78155 Phone: 830-379-1580 Fax: 830-379-9544 Customer Service Toll Free: 1- 866-601-5430 For European sales office numbers and a full address list, please go to: http://www.hexcel.com/contact/salesoffices Copyright 2014 Hexcel and Hexcel logo are registered trademarks of Hexcel Corporation, Stamford, Connecticut. HexForce is a trademark of Hexcel Corporation, Stamford, Connecticut. June 2014

15MC848127050_TDS.pdf

Document No.
MKT-002
PE 80Dtex
N/A
Layer
-45
+45
Liner (Upper)
Stabilisation Thread – 90
Stabilisation Thread – 0 68tex Glass
N/A
Stitch Fibre
MC8481270
Sigmatex Product Data Sheet
Description410GSM/-45+45/T700SC 12K 50C/1270mm
Fabric StyleBi-Axial
From global locations, Sigmatex supplies carbon fibre textiles including 3D, Spread Tow, Innegra, Recycled, Unidirectional, Multiaxial, and 2D across a broad
spread of industries ranging from the world s top supercar manufacturers to aerospace companies. In all cases, Sigmatex helps its customers to achieve
improved product performance through lightweight strength. Sigmatex was established in 1986 and has specialised in converting carbon fibre since then.
For more information see www.sigmatex.com or contact a member of the sales team on +44 (0) 1928 570 050
This is an uncontrolled document and may be subject to change.
*Tolerances on fabric properties can be provided on request.
“Layer” Mass
Warp Bow 5mm per 1m length (max)
“Stitch” Mass 6
As per customer requirements
Width 1270 mm
“Stabilisation” Mass
gsm
Typical Length (lm)See Above
“All-Up” Mass 410 gsm
Property
Bow
Nominal Weight (gsm)
T700SC 12K 50C 200
Fibre Description
T700SC 12K 50C 200
Spacing 0 22.5mm
Spacing 90 N/A
Stitch Pattern Chain
Axis angle 1.5 per m width
See Above
Construction Verify
Thickness Verify
N/ALiner (Lower)
Requirement
Fabric Properties
Property Nominal Units
Printed versions of this document
may not be at the latest issue level.
Author:
K. Gardner / G. Shaw
Page 1 of 1
MKT-002 Iss.002 Fabric Data Sheet

15M1028450_TDS.pdf

HexPly

M10E
Epoxy Resin System
Product Data Sheet
Description
HexPly

M10E is an epoxy resin system preimpregnated into aramid, glass or graphite multiaxial fabrics and
unidirectional fibers. HexPly

M10E prepregs are recommended for the production of low cost, large thick-
sectioned industrial structures.
Features
Flexible Cure Cycle (185 F to 300 F)
Vacuum Bag or Autoclave Cure
High Flow, Low Viscosity System
Medium to High Tack
Can be Stored at Room Temperature for 60 Days
Optically Clear Resin
Properties
Glass transition temperature: Dry, 241 F, Wet, 194 F
Resin density 1.19
Barcol Hardness 33
Availability
Form
Hexcel
Designation
Fiber
Fiber Areal
Wt. G/m
2
Weave
Count
Warp x Fill
Available Widths
Standard Widths
in (cm)
Fabric PW 282 3K 197 Plain weave12 by 12 50
Graphite UD
AS3C-S
150-300 GSM
AS3C-S
12K
150-300 12 , 24
Physical Properties
Property Carbon Tapes
Tensile and compressiveM10E 37% AS3C-S, 300 GSM
1
Copyright 2020 Hexcel Corporation All Rights Reserved.

Product Data Sheet
2
Mechanical Properties
Property Temperature Condition Carbon Tapes
Tensile Strength Room Temp. Dry 293 ksi
Tensile Modulus Room Temp. Dry 17.6 Msi
Tensile Strain Room Temp. Dry 1.54%
Compression Strength Room Temp. Dry 154 ksi
Compression Modulus Room Temp. Dry 17.0 Msi
Compression Strain (calculated) Room Temp. Dry 0.91%
Cure Cycle
185 F, 14 hours
200 F, 120 minutes
250 F, 30 minutes
300 F, 8 minutes
Cure Procedure
Vacuum bag or autoclave cure using ramp rate of 2-5 F per minute. Recommend hold at 250 F for 30 minutes.
Storage (maximum, from date of manufacture)
At 0 F, 18 months
At 41 F, 6 months
At 72 F, 2 months
FTI-329-MY20
HexPly

M10E
epoxy resin system
2020 Hexcel Corporation All rights reserved. Hexcel Corporation and its subsidiaries ( Hexcel ) believe that the technical data and other information
provided herein was materially accurate as of the date this document was issued. Hexcel reserves the right to update, revise or modify such technical data and
information at any time. Any performance values provided are considered representative but do not and should not constitute a substitute for your own testing
of the suitability of our products for your particular purpose. Hexcel makes no warranty or representation, express or implied, including but not limited to the
implied warranties of merchantability and fitness for a particular purpose, and disclaims any liability arising out of or related to, the use of or reliance upon any of
the technical data or information contained in this document.
For more information
Hexcel is a leading worldwide supplier of composite materials to aerospace and industrial markets.
Our comprehensive range includes:

For U.S. quotes, orders and product information call toll-free 1-800-688-7734. For other worldwide sales office
telephone numbers and a full address list, please go to:
https://www.hexcel.com/contact
HexTow

carbon fibers
HexForce

reinforcements
HiMax

multiaxial
reinforcements
HexPly

prepregs
HexMC

-i molding compounds
HexFlow

RTM resins
HexBond

adhesives
HexTool

tooling materials
HexWeb

honeycombs
Acousti-Cap

sound
attenuating honeycomb
Engineered core
Engineered products
Polyspeed

laminates
& pultruded profiles
HexAM

additive manufacturing

15M1028250_TDS.pdf

HexPly

M10E
Epoxy Resin System
Product Data Sheet
Description
HexPly

M10E is an epoxy resin system preimpregnated into aramid, glass or graphite multiaxial fabrics and
unidirectional fibers. HexPly

M10E prepregs are recommended for the production of low cost, large thick-
sectioned industrial structures.
Features
Flexible Cure Cycle (185 F to 300 F)
Vacuum Bag or Autoclave Cure
High Flow, Low Viscosity System
Medium to High Tack
Can be Stored at Room Temperature for 60 Days
Optically Clear Resin
Properties
Glass transition temperature: Dry, 241 F, Wet, 194 F
Resin density 1.19
Barcol Hardness 33
Availability
Form
Hexcel
Designation
Fiber
Fiber Areal
Wt. G/m
2
Weave
Count
Warp x Fill
Available Widths
Standard Widths
in (cm)
Fabric PW 282 3K 197 Plain weave12 by 12 50
Graphite UD
AS3C-S
150-300 GSM
AS3C-S
12K
150-300 12 , 24
Physical Properties
Property Carbon Tapes
Tensile and compressiveM10E 37% AS3C-S, 300 GSM
1
Copyright 2020 Hexcel Corporation All Rights Reserved.

Product Data Sheet
2
Mechanical Properties
Property Temperature Condition Carbon Tapes
Tensile Strength Room Temp. Dry 293 ksi
Tensile Modulus Room Temp. Dry 17.6 Msi
Tensile Strain Room Temp. Dry 1.54%
Compression Strength Room Temp. Dry 154 ksi
Compression Modulus Room Temp. Dry 17.0 Msi
Compression Strain (calculated) Room Temp. Dry 0.91%
Cure Cycle
185 F, 14 hours
200 F, 120 minutes
250 F, 30 minutes
300 F, 8 minutes
Cure Procedure
Vacuum bag or autoclave cure using ramp rate of 2-5 F per minute. Recommend hold at 250 F for 30 minutes.
Storage (maximum, from date of manufacture)
At 0 F, 18 months
At 41 F, 6 months
At 72 F, 2 months
FTI-329-MY20
HexPly

M10E
epoxy resin system
2020 Hexcel Corporation All rights reserved. Hexcel Corporation and its subsidiaries ( Hexcel ) believe that the technical data and other information
provided herein was materially accurate as of the date this document was issued. Hexcel reserves the right to update, revise or modify such technical data and
information at any time. Any performance values provided are considered representative but do not and should not constitute a substitute for your own testing
of the suitability of our products for your particular purpose. Hexcel makes no warranty or representation, express or implied, including but not limited to the
implied warranties of merchantability and fitness for a particular purpose, and disclaims any liability arising out of or related to, the use of or reliance upon any of
the technical data or information contained in this document.
For more information
Hexcel is a leading worldwide supplier of composite materials to aerospace and industrial markets.
Our comprehensive range includes:

For U.S. quotes, orders and product information call toll-free 1-800-688-7734. For other worldwide sales office
telephone numbers and a full address list, please go to:
https://www.hexcel.com/contact
HexTow

carbon fibers
HexForce

reinforcements
HiMax

multiaxial
reinforcements
HexPly

prepregs
HexMC

-i molding compounds
HexFlow

RTM resins
HexBond

adhesives
HexTool

tooling materials
HexWeb

honeycombs
Acousti-Cap

sound
attenuating honeycomb
Engineered core
Engineered products
Polyspeed

laminates
& pultruded profiles
HexAM

additive manufacturing

15HMGP20050_TDS.pdf

HexForce
TM
HMGP200-P ZB
Carbon Fabric

Style HMGP200- P ZB US System
Type of Yarns Warp Yarn: HEXCEL HM63 12K GP
Fill Yarn: HEXCEL HM63 12K GP
Fabric Weight, Dry 5.89 oz/yd
2
200 g/m
2

Weave Style Plain
Finish ZB
Construction
Nominal Construction Warp Count: 6.0/in 15.24/cm
Fill Count: 6.0/in 15.24/cm

Important
All information is believed to be accurate but is given without acceptance of liability. All values have been generated
from limited data. The values listed for weight, thickness and breaking strengths are typical greige values, unless
otherwise noted. Users should make their own assessment of the suitability of any product for the purpose required.
All sales are made subject to our standard terms of sales which include limitations on liability and other important
terms. The fabric style listed may not be available from inventory and minimum order quantities may apply.
For More Information
Hexcel is a leading worldwide supplier of composite materials to aerospace and other demanding industries.
Our comprehensive product range includes:
Carbon Fiber
Reinforced Fabrics
Carbon, Glass, Aramid and Hybrid Prepregs
RTM Materials
HexTOOL

composite tooling material
Structural Film Adhesives
Honeycomb Cores
Engineered Core

1913 North King Street
Seguin, Texas 78155
Phone: 830-379-1580
Fax: 830-379-9544
Customer Service Toll Free: 1- 866-601-5430
For European sales office numbers and a full address list, please go to:
http://www.hexcel.com/contact/salesoffices

Copyright 2014 Hexcel and Hexcel logo are registered trademarks of Hexcel Corporation, Stamford, Connecticut.
HexForce is a trademark of Hexcel Corporation, Stamford, Connecticut.
June 2014

15I9F9230A_TDS.pdf

Inspired by Innovation :: Driven by Excellence

BGF INDUSTRIES, INC.
3802 Robert Porcher Way Greensboro, North Carolina 27410 USA
336-545-0011 fax: 336-545-0233 toll free: 800-476-4845
www.bgf.com
info@bgf.com

STYLE: 7590
FINISH: 504 Volan
WEAVE: 2×2 RH Twill
WARP YARNS: ECG 75 1/2
FILL YARNS: ECG 75 1/2
COUNT (ends x picks/inch): 18×18
WEIGHT (osy): 5.8

Information herein is based on BGF’s testing procedures and standards which we believe are accurate and reliable. BGF
makes no warranties as to any other characteristics of the products, their fitness for a particular purpose of the customer or
infringement of any patent for any particular use by the customer.

PRODUCT INFORMATION

STYLE 7590