A Handy & Harman Company

JPS Composite MaterialsCorporate Headquarters and US Operations

2200 South Murray AvenueP.O. Box 2627

Anderson, SC, 29622(864) 224-3506

(800) 431-1110 Toll Free(800) 288-0577 Toll Free

(864) 260-6581 Fax

Table of ContentsCompany........................................................................ 1Locations....................................................................... 1Conditions of Sales....................................................... 2Parameters for Fabric Selection.....................................3Fiberglass Yarn Nomenclature....................................... 4Glass Composition......................................................... 4Glass yarn filament sizes & counts................................ 6Design Considerations for Glass Fabric Selection.........6Manufacturing Process Overview...................................9Weave Patterns............................................................10Specifications & Standards.......................................... 14

FIBERGLASS PRODUCTS......................................... 15Physical Properties of E-glass..................................... 15Physical Properties of S-2 ® Glass..............................16Fiberglass Fabric Applications..................................... 17Fiberglass Fabric Finishes........................................... 18

FIBERGLASS FABRIC CONSTRUCTIONS................ 20Fiberglass Fabric Weight Index....................................31Fiberglass Fabric Thickness Index...............................34

ASTROQUARTZ ® PRODUCTS................................. 37Properties of Astroquartz ® Fibers............................... 37Physical Properties of Fused Quartz............................38Astroquartz ® Applications and Design Considerations............................................ 38Astroquartz ® II & III Fabric Finishes........................... 40Astroquartz II ® Chopped Fiber................................... 41

ASTROQUARTZ ® II & III FABRICS........................... 42Astroquartz ® Mat Style No. 550................................. 43Astroquartz ® II Roving............................................... 43Astroquartz ® II Sewing Thread................................... 44Astroquartz ® II Yarn................................................... 45

POLYMER FIBER FABRIC PRODUCTS..................... 46Physical Properties of Para-Aramids........................... 46Physical Properties of UHMWPE.................................47Advanced Materials Applications................................. 48

ii

Advanced Fabrics Nomenclature...................................48Finishes for Advanced Materials..................................49

Aramid Fabric Constructions........................................50Aramid Fabric Weight Index........................................ 57Aramid Fabric Thickness Index................................... 59Engineered Aramid Fabrics......................................... 61

Dyneema Fabrics........................................................ 62

Spectra Fabrics............................................................63

Carbon Fabrics............................................................ 64Carbon Fabric Constructions....................................... 65

Technical References - English................................... 66

Technical References - Metric......................................67Selected Conversions & Formulae.............................. 68

Notes........................................................................... 69

iii

1 Company

JPS Composite Materials is the world’s leading manufacturer of high strength fiberglass, Astroquartz ®, aramid, carbon, and specialty reinforcement fabrics.

Our materials are used extensively in composite reinforcing, insulating, and safety applications. JPS fabrics are used in consumer and industrial electronics, aerospace interior and exterior structures, advanced commerical and military radomes, in marine and surf applications, sporting goods, and other advanced composites, and as ballistic protection.

Our materials are readily adaptable to unlimited applications!

Direct customer access to customer service:

1-800-431-11101-800-288-0577(864) 260-6581 Fax

For further information, write to JPS Composite MaterialsPO Box 2627, Anderson, SC, 29622dhudgens@jpscm.com

LocationsAnderson, South CarolinaCorporate HeadquartersAerospace Composite, Astroquartz ®, Aramid, and Specialty Fabrics

Statesville, North CarolinaElectrical Laminate E-glass Fabrics,Lightweight Advanced and Aerospace Composite Fabrics,Carbon Fabrics

2

Conditions of SalesAll sales of JPS products are subject to the terms and conditions of JPS’ standard confirmation of order.

All statements herein are expressions of opinion which the Seller believes to be true and correct. Seller expressly disclaims liability for factual accuracy of such opinions and hereby advises Buyer to investigate each situation on an individual basis before taking action based on Seller’s expression of opinion.

Statements concerning possible use of our products are not intended as recommendations for their use in the infringement of any patent. No patent warranty of any kind, expressed or implied, is made or intended.

For further information, write to JPS Composite MaterialsPO Box 2627, Anderson, SC, 29622(800) 431-1110, (800) 288-0577, (864) 260-6581 Fax

PLEASE NOTE: Because of the many variables associated with producing industrial reinforcement fabrics (yarn type, fabric construction, widths, finishes and other facts), the technical data and other information contained on these pages are intended as a general guide only. The data contained herein is subject to change at the Seller’s discretion without notification unless specifically prohibited by specific purchase specifications.

A Handy & Harman Company

3

Parameters for Fabric SelectionIn selecting a woven fabric for industrial applications a number of design parameters must be considered. These are broken down into five basic variables: Yarn Weight, Yarn Thickness, Yarn Count, Weave Pattern, and Fabric Finish.

Yarn weight and yarn count determine the majority of the physical properties of the fabric. Yarn count is defined as the number of warp yarn ends (lengthwise) and filling yarn picks (widthwise) used per inch.

The weave pattern determines the stiffness or drapability of the fabric. The pattern will also have an influence on overall thickness. For composite applications there are six basic patterns: Plain, Basket, Leno, Four Harness Satin (Crowfoot), Eight Harness Satin, and Twill.

The fabric finish is the surface chemistry applied to the fabric post weaving. Finishes are generally applied to promote adhesion between the fabric and any resin coatings. They may also serve to add stiffness, prevent moisture uptake, and wear damage caused by handling.

Glass YarnYarn determines the majority of the end fabric properties,including the fabric weight, thickness, and strength.

The yarn properties are determined by the chemical composition, the number of input filaments per yarn strand, the number of yarn strands twisted or plied together, and the overall denier (weight) of the final input yarn.

Glass FormulationsGlass fibers are made from different formulations: “E” is the most common all-purpose glass. Other types include “S”, “T”, and “L”, among others. Astroquartz ® products are the purest form of silica commercially available.

4

COMPOSITION OF TYPICAL GLASSES (%) by weight

“E” “S”, “T” “Astroquartz ® Ingredient Glass Glass II & III”

Silicon Dioxide 52-60 64-66 99.99 Calcium Oxide 16-25 - - Aluminum Oxide 12-16 24-26 - Boron Oxide 8-13 - - Sodium and Potassium Oxide 0-1 - - Magnesium Oxide 0-6 9-11 -

Filament/Yarn NomenclatureAn exact system for identifying fiberglass textile yarns is required because of the wide variety of available types. The nomenclature consists of two basic parts. The alphabetical portion describes the composition and construction. The numerical describes the weight and number of yarns twisted and plied together.

As an example:

Glass Number ofComposition Single StrandsE=Electrical Filament in ContinuousS=High Strength Diameter Filament Yarns

E C G 150 1/2

Type of Yarn Strand Number of C=Continuous Count Strands Filament Yardage/Lb Plied (in Hundreds) TogetherThe above describes the basic strand by composition, type and diameter. The numbers identify strand weight and construction. The above description would be for ECG 150 1/2 yarn, or more simply G-150 1/2, used in style 1581 fabric. The S-glass version for style 6581 fabric would be SCG 150 1/2, where “S” denotes S-glass. The non-twisted equivalent for 7781 would be ECDE 75 1/0.

5

The strand count is the first series of numbers following the letters. It indicates approximate yardage per pound, in hundreds. The number of yards in one pound of single yarn strand can be found by multiplying the strand count by 100.

The second series of numbers designates the number of plies in continuous filament yarns. The first digit in the second digit series indicates the number of single strands twisted together. Untwisted single strands are commonly referred to as “singles” yarn and are designated as 1/0.

The second digit in the second series, separated from the first digit by a diagonal line, designates the number of strands that are plied together. To find the total number of strands in a yarn, multiply the two numbers (0 multiplied as 1). A typical nomenclature for a continuous yarn:

ECG 150-1/2 Where: E = E-glass

C = Continuous filament

G = Average filament diameter (see table, page 6)

150 = 15,000 Yd/Lb (Nominal) of basic “singles” strand

1/2 = One continuous filament yarn strand consisting of two strands plied together (1X2)

The approximate yards per pound of fabricated yarn can be found by dividing the strand count, multiplied by 100, by the number of strands.

Therefore, ECG 150 1/2 contains: 150 x 100 1 x 2

The results of this computation must always be considered approximate, as yards per pound may be reduced slightly in the twisting and plying operations.

= 7500 yds/lb for fabricated yarn

DESCRIPTION OF CONTINUOUS FILAMENT GLASS FIBERS Filament Strand Number Filament Diameter Count of Name mils microns (x100=yd/lb) Tex Filaments

B 0.15 3.8 150 33 1224

C 0.15 3.8 150 33 816

D 0.23 5.0 1800 2.75 51 900 5.5 102 450 11 204 225 22 408 DE 0.25 6.0 150 33 408 75 66 816 50 99 1224 37 134 1632

E 0.29 7.0 225 22 204

G 0.36 9.0 150 33 204 75 66 408 37 134 816

H 0.43 10 25 198 816

K 0.51 13 75 66 204 37 134 408 25 198 608 18 275 816

DESIGN CONSIDERATIONS FOR GLASS FABRIC SELECTIONThere are five basic design variables to consider when choosing fabric for industrial use: thickness, aerial weight, yarn size, construction, finish.

ThicknessGlass fabrics are available in thicknesses ranging from ~0.001” to ~0.060”.

6

7

WeightFabric weights are typically measured in ounces per square yard (osy) or grams per square meter (gsm). Glass fabrics are available from about 0.50 osy up to about 52 osy (17 gsm to 1773 gsm.)

ConstructionConstruction refers to the fabric pattern, which is both the number of warp yarns per inch (machine direction, ends) and fill yarns per inch (cross-machine direction, picks),and the pattern of interlacing used (plain, twill, satin, etc).

Yarn Size (denier or weight)Fabric weight and thickness are determined by the input yarn size (denier or weight).

FinishThe finish is the chemical composition of the surface of final fabric. Organic coatings are applied (or removed) to make the fabric more suitable for future resin coating and end use performance requirements.

FABRIC CREATION

Yarn Preparation: Twisting/PlyingThis process serves to control the yarn strength, diameter, weight, and flexibility.

Filaments are twisted and or plied based on the end fabric specification requirements. Most glass fabrics are woven from singles yarns (1/0).Some notable exceptions including styles 108, 120, and 1581.

WarpingWarping is the laying of the machine direction fibers in parallel order. This creates the warp, or machine direction, lof the fabric.

A specified number of yarns per inch are drawn from a

creel and wound on a warp beam. Several “section” beams are then combined to provide the designated number of yarns per inch required in the fabric specification.

Slashing/CombiningThe section beams from warping are combined during the slashing process to create a warp beam (aka: loom beam). This entire system of parallel threads is wound onto one large beam to become the “warp”, or machine direction, of the fabric.

An additional yarn binder is applied to the warp yarns during the slashing process. The additional binder helps to improve fabric surface quality by providing extra protection to the warp yarns during the weaving process.

EnteringThe entering operation draws the warp yarns into to the loom, setting up the weave pattern, yarn spacing and thread counts. The warp yarns are threaded through the harnesses and reed. The entire warp beam-harness-reed unit is then transferred to the loom to begin weaving.

WeavingWeaving is the interlacing of filling (cross machine) yarns through warp (machine direction) yarns in a predetermined pattern, including yarn counts, yarn spacings, over/under sequences and predetermined intersecting angles.

Cleaning and FinishingDependent on the end fabric use, specialty chemical finishes may be applied to the fabric surface. The loom state (greige) fabric surface must first be cleaned. This is accomplished via either heat exposure or chemical washing. Most glass fabrics are ‘heat cleaned’, most polymer based and specialty fabrics are chemically scoured. The specialty finish is applied post cleaning.

8

1. Yarn Prep and Warping

Yarn Creel SectionBeam

Section Beams

SlashingBinder Addition

Oven WarpBeam

2. Slashing/Combining

5. Heat Cleaning/Chemical Scouring

3. Entering

WarpBeam

Reed &Harnesses

4. Weaving

WarpBeam

Reed &Harnesses

GreigeFabric

6. Finishing

GreigeFabric

FinishedFabric

Accumulator**not necessary

Accumulator**not necessary

Oven

Manufacturing Process Overview

9

10

Finishes most commonly act as coupling agents to improve resin wet-out and bonding. Finishes may also be applied to improve water and wear resistance, high temperature performance..

JPS offers a wide range of existing finishes. We do develop specialty and exclusive finishes based on customer input. For more information please contact us.

Weave PatternsThe matching of yarn, weave pattern and finish for a particular application is an exacting science. Because glass, carbon, aramid and specialty fabrics are highly engineered, the right combination of fabric weight, thickness and construction is essential in selecting the proper fabric. Selecting the right reinforcement fabric for any requirement can be simplified by calling us. Our specialized experience can aid in selecting a reinforcement fabric suited to your requirements.

All standard of fabric weaves presented here can be produced with fiberglass, aramid, Astroquartz ®, polymer, specialty and carbon yarns.

The six most common fabric patterns are presented here. Other fabric patterns are available on request; as well as through development.

Plain Weave fabrics tend to be the most stable pattern, followed by Leno, Basket Weave, 4H Satin, 8H Satin fabrics.

In terms of drape or conformability, 8H Satin is the mostconformable, followed by the 4H Satin, Basket Weave, Plain Weave and Leno fabrics.

11

Plain Weave

The plain weave consists of yarns interlaced in an alternating pattern, one over and one under every other yarn. The plain weave provides good fabric stability. It is the primary fabric \used in the electronics and coating industries.

Basket Weave

The basket weave is similar to the plain weave, except that two or more filling yarns are alternately interlaced over and under one another. The basket weave is more pliable, flatter, and stronger than the plain weave, but is not as stable as a plain weave.

12

Leno

The leno weave is used where relatively low aerial weights are desired but specific thicknesses must be maintained. The leno weave pattern locks the yarns in place by crossing two or more warp threads over each other and interlacing with one or more fill threads. Leno weave patterns are common in EIFS applications and to set bond line thicknesses for adhesives and tapes.

Four-Harness Satin (Crowfoot)

The four-harness satin relies on a three by one interlacing, pattern. The fill yarn floats over three warp yarns and under one. The four-harness satin weave is more pliable than the plain weave and is easier to conform to curved surfaces typical in reinforced plastics.

13

Eight-Harness Satin

The eight-harness satin is similar to the four-harness satin except than one filling yarn floats over seven warp yarns andunder one. This is a very pliable weave and is used for forming curved surfaces.

2x2 Twill

The twill is used where tightly woven fabric with high density is required. The twill weave is characterized by a diagonal rib or twill line. The warp yarn floats over two consecutive picks, permitting more yarns per unit area.

Specifications and StandardsJPS fabrics are designed to meet the requirements of a wide range of applications. Listed below is a partial offering of the standards and specifications we manufacture towards. For adherence to a specific standard or specification not listed please contact customer service or technical support.

AMS-3824 - Glass Cloth, Finished for Resin Laminates

AMS-3846 - Quartz Cloth, Finished for Resin Laminates

AMS-3902 - Para-Aramid Cloth for Structural Composites

AMS-C-9084 - Glass Cloth, Finished for Resin Laminates

ASTM-D-579 - Greige Woven Glass Fabrics

ASTM-D-1668 - Standard Specification for Glass Fabrics

ASTM-D-4029 - Standard Specification for Finished Glass Fabrics

BMS 9-3 - Boeing requirements for E-Glass Fabrics

BMS 9-8 - Boeing requirements for carbon Fabrics

BMS 9-17 - Boeing requirements for Intermediate Modulus Carbon Fabrics

IPC-4412 - Standard Specification for Glass Fabrics for Use in Printed Circuit Boards

MIL-DTL-62474 - Aramid-Reinforced-Plastic Composites

MIL-PRF-64154 - Glass-Reinforced-Phenolic Composites

MIL-R-7575 - Glass-Reinforced-Polyester Composites

MIL-R-9300 - Glass-Reinforced-Epoxy Composites

MIL-Y-1140 - Greige Woven Glass Fabrics

14

FIBERGLASS PRODUCTS

Physical Properties of E-glass Fiber

Approximate Chemistry*SiO ........................................................................52-56%CaO........................................................................ 16-25%Al O ......................................................................12-16%B O ......................................................................... 5-10%MgO............................................................................ 0-5%NaO .......................................................................... 0-1%KO .............................................................................0-1%Other Elements...........................................................0-2%

Physical Properties*Density..........................................................2.54-2.60 g/ccRefractive Index........................................... 1.547 to 1.562Mohs Hardness..............................................................6.5

Mechanical Properties*UTS (room temp).............................................3.4-3.5 GPaBreaking Strain......................................................4.5-5.0%Young’s Modulus................................................ 65-75 GPaShear Modulus................................................... 28-32 GPaPoisson’s Ratio........................................................... 0.200

Thermal Properties*CTE (-30ºC to 250ºC)......................................5.4 µm/m-ºCSpecific Heat Capacity............................ 0.80-1.03 kJ/kg-KThermal Conductivity....................................1.0-1.3 W/m-KSoftening Point........................................................≤ 845ºC

Electrical Properties*Dk @ 1 MHz.................................................................. 6.6Dk @ 10 GHz................................................................. 6.1Df @ 1 MHz................................................................0.003Df @ 10 GHz..............................................................0.004Volume Resistivity........................................4.02 Ω-cmSurface Resistivity....................................... 4.20 Ω-cmDielectric Strength................................................103kV/cm*All values approximate. Actual values may vary, for further info contact JPS.

2

22

2 32 3

1015

1016

15

Physical Properties of S-GlassApproximate Chemistry*SiO .........................................................................64-66%Al O .......................................................................24-26%MgO........................................................................... 9-11%Other Elements.........................................................0-1.2%

Physical Properties*Density...........................................................2.46-2.49 g/ccRefractive Index............................................ 1.520 to 1.525Mohs Hardness...............................................................6.5

Mechanical Properties*UTS (room temp)..............................................4.6-4.8 GPaBreaking Strain...................................................... 5.4-5.8%Young’s Modulus................................................ 85-90 GPaShear Modulus................................................... 33-37 GPaPoisson’s Ratio........................................................... 0.230

Thermal Properties*CTE (-30ºC to 250ºC)...................................... 2.9 µm/m-ºCSpecific Heat Capacity............................. 0.74-0.82 kJ/kg-KThermal Conductivity.................................... 1.1-1.4 W/m-KSoftening Point......................................................≤ 1055ºC

Electrical Properties*Dk @ 1 MHz....................................................................5.3Dk @ 10 GHz..................................................................5.2Df @ 1 MHz.................................................................0.002Df @ 10 GHz...............................................................0.007Volume Resistivity........................................0.905 Ω-cmSurface Resistivity....................................... 0.886 Ω-cmDielectric Strength................................................130kV/cm

*All values approximate. Actual values may vary, for further info contact JPS.

10131013

22 3

16

Fiberglass Fabric ApplicationsFiberglass fabrics are used in a wide range of industrial applications, some of which are outlined below.

Aerospace ApplicationsFiberglass is used for interior cabin structures including seats, luggage bins, bulkheads, lavatories, wall panels, and in honeycomb structures. Other applications include gasketing, as galvanic barriers between carbon and metal, for structural parts, and in support of radomes. JPS is BMS, AMS, SAE and MIL spec approved for your needs.

Electrical ApplicationsFiberglass fabrics can be found in printed circuit boards, antennas, high voltage generators, transformers, switches, cables and many other electrical applications.

Structural ApplicationsFiberglass fabrics are used as reinforcements in highly engineered composite materials in many of the world’s leading aircraft, automobiles, buildings, and roadways,

Recreational ApplicationsJPS fiberglass is found in many recreational composites, including in high performance racecars and motorcycles, bicycles, bats, racquets, hockey sticks, and in high end surf and snow boards.

Thermal InsulationThe U.S. Navy, commercial shipyards, the automotive, and aerospace industries all use fiberglass almost exclusively for pipe lagging, thermal pad cover, thermal protection, and insulation applications.

General Industrial ApplicationsFiberglass fabrics can be found in window shades, vapor barriers, movie screens, packaging tapes, awnings, protective clothing, gaskets, conveyor belts, food cookingapplications, and countless other products that improve our lives daily.

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Fiberglass Fabric Finishes

Fiberglass fabrics are available with a variety of finishes and treatments. The most common finishes are listed here, forspecific applications, or to develop a custom finish for yourapplication please contact customer service or your technical support representative.

Finish Functionality: Name Primary Secondary Notes Greige Uncoated Phenolic Loom state fabric with yarn binders

Caramelized Uncoated PTFE Loom state fabric, (210) partially volatized

F3 Polyester Epoxy Volan, green tintF12 Silicone Neutral pH F16 Polyester Epoxy Volan, green tint 112 Uncoated Phenolic Fully heat cleaned BMS 9-3 Listed

CS-309 Polyimide Epoxy, BT Silane Finish CS-310 Epoxy Silane Finish BMS 9-3 Listed

CS-550 PE, Epoxy Phenolic Volan, green tint

CS-718 Epoxy Silane Finish CS-616 Melamine Silane finish, tan

CS-724 Epoxy Silane Finish BMS 9-3 Listed

CS-745 Epoxy BT, Cynate Silane Finish Ester, PI

CS-767 Epoxy, BMI, Silane Finish Polyimide, Phenolic, BMS 9-3 Listed Cynate Ester SBR

18

Finish Functionality: Name Primary Secondary Notes S-910 Polyester High clarity for surf S-912 Polyester Epoxy High clarity for surf A-1100 Phenolic Epoxy Silane finish BMS 9-3 Listed

A-1100S Phenolic Epoxy Recommend for hand layup, BMS 9-3 Listed Z-6040 Epoxy Phenolic Common base silane 9464 Uncoated Epoxy Antimony-fee Hull Board

9465 Uncoated Epoxy Higher flame retardant Hull Board

9466 Uncoated Epoxy Standard Hull Board9827 Epoxy Polyimide Silane finish9837 Vinyl Ester Polyester Vinyl silane finish

Great White Polyester Highest clarity for surfVolan Polyester Epoxy Volan finish, green tint, BMS 9-3 Listed

Fiberglass Fabric Finishes (cont.)

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37

ASTROQUARTZ ® PRODUCTSAstroquartz ® is a registered trademark of JPS Industries

JPS has been weaving the 99.99% pure silica fabric since 1964. Astroquartz ® is used in many of the world’s most advanced composite applications. This includes usage in the manned and unmanned space programs, as stealth supporting materials, as radomes for superior signal integrity,and internet connectivity on commercial airliners.

Astroquartz ® is the leader when it comes to low dielectric,high strength, and high thermal reliability composite reinforcements.

Astroquartz II ® &Astroquartz III ® PropertiesAstroquartz ®, Astroquartz II ® and Astroquartz III ® are composed of identical raw materials. Astroquartz ® has been discontinued in favor of Astroquartz II ® and Astroquartz III ®. Improved manufacturing and handling technologies have allowed Astroquartz II ® and Astroquartz III ® to become more robust and cost effective. All represent unparalleled quality, purity, and performance. JPS and Astroquartz ® innovation gives new flexibility to your design opportunities.

Properties of Astroquartz ® FibersTensile Strength - Virgin Single Filament.............6.0 GPa (870 ksi)Tensile Strength - Impregnated Strand on 20 End Roving (ASTM D-2343).......................3.6 GPa (530 ksi)Young’s Modulus....................................... 72 GPa (10 msi)Poisson’s Ratio.............................................................0.16Density................................................................. 2.2 g/cm Silica Content (exclusive of yarn binder).................99.99%Fiber Diameter - Astroquartz II ®..................................9µmFiber Diameter - Astroquartz III ®...............................14µm

3

38

Physical Properties of Fused QuartzMechanical PropertiesDensity............................................2.2 g/cm or 0.79 lb/m Hardness (Mohs Scale).....................................................7

Electrical PropertiesDielectric Constant (Dk) - 1 MHz..................................3.70Dielectric Constant (Dk) - 10 GHz................................ 3.74Dissipation Factor (Df) - 1 MHz.................................0.0001Dissipation Factor (Df) - 10 GHz.............................. 0.0002

Thermal PropertiesLinear Expansion Coefficient..............................0.54 x 10Specific Heat @ 20ºC (J/gK)................................ 7.5 x 10Thermal Conductivity (W/mK)...................................... 1.38Strain Point (Log n = 14.6).....................1070ºC (1958ºF)Annealing Point (Log n = 13)................. 1220ºC (2084ºF)Softening Point (Log n = 7.6).................1700ºC (3092ºF)Note: n = Viscosity in Poise

Optical PropertiesRefractive Index @ 15ºC...........................................1.4585Dispersion....................................................................... 67Field of Transparency (µm).................................. 0.2 to 4.0

Astroquartz ® Applications and Design ConsiderationsAstroquartz ® fabrics offer better solutions when high strength, low dielectric loss and high heat resistance is required.

The aerospace industry relies on Astroquartz ® fiber productsmade from pure fused silica (99.99% SiO ) to produce an outstanding, reproducible reinforcement material.

There are five basic design variables to consider when choosing Astroquartz ® fabrics:

2

3 3

-6

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2

39

Astroquartz ® Applications and Design Considerations (cont.)

ThicknessQuartz and composite fabrics are available in thicknessesranging from 0.003” to 0.027” (0.13-0.69 mm).

WeightThe weight for Astroquartz ® fabrics range from 2.0 to 19.5 ounces per square inch (128 to 660 gsm).

ConstructionConstruction is the number of warp and fill yarns per inch (machine and cross-machine direction) and the fabric pattern. This helps determine the thickness, weight, drapability, and overall performance of the fabric.

Yarn SizeYarn size is a major factor in determining the weight and thickness of the fabric. The yarn size, twist and ply countswill also play a large role in determining the overall strength of the woven fabric. For specific applications, one yarn may be selected over another to the advantage of the performance characteristics.

FinishThe Astroquartz ® fabrics can be coated with a coupling agent, called the finish, to assist resin wet out and to improve the strength of the fiber to resin interface. This hasthe effect of improving the mechanical, thermal and electrical performance characteristics of the final part. Please contactJPS technical or customer service for assistance in choosingthe correct fabric finish for your application.

Finish Functionality: Name Primary Secondary Notes S-928 Epoxy Epoxy functional silane 1059 HT/ Polyimide Thermo- Formulated for high2059 HT/ plastic temperature and3059 HT matrices moisture resistance9779 Epoxy Bismaleimide Amino-silane Cynate Ester

9827/ Epoxy Polyimide, Recommended for2827/ Bismaleimide electronic and 3827 aerospace applications9836/ Epoxy Bismaleimide Scoured fabric to2836/ to remove most 3836 organic binder components

9837/ Polyester Vinyl Ester Recommended for2837/ Epoxy, resins cured by vinyl 3837 Cynate Ester addition

Astroquartz ® II & III Fabric Finishes A partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPS.

40

41

Astroquartz II ® Chopped FiberAstroquartz II ® chopped fiber is made by cutting continuous filaments of high purity, extremely fine quartz to a predetermined length. Fiber composition is 99.99% SiO (silica) exclusive of binder.

Astroquartz II ® chopped fibers are widely used in reinforced plastics, molding compounds and ceramic composites. The chopped fibers add thermal resistance and improved ablation to the final part.

Type 556 Chopped FiberFiber Lengths* Astroquartz II ® chopped fiber with an from 1/8” to 1” aminosilane binder. Compatible with epoxy, phenolic and some polyimide resins.

* Due to the nature of the cutting process, cut lengths may vary slightly.

Standard Packaging

1 lb packages packed loosely in clear polyethylene bags.

Order Requirements and Lead Times

Please contact JPS to confirm availability and lead time.

Dependent on available inventory the minimum order requirement is approximately 60 lbs. Please allow 8-12 weeks for processing.

2

42

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43

Astroquartz ® Mat Style No. 550SpecificationsLength...................................................1000 mm (39.37 in)Width.......................................................500 mm (19.69 in)Area............................................ 0.5 m per sheet (5.38 ft )Thickness........................................................5 mm (0.2 in)Weight.................................................. 78 g/m (2.3 oz/yd )Density.................................. 0.016 g/cm (1 lb/ft - approx.)

HandlingAstroquartz ® s/550 mat is impregnated with a polyvinyl alcohol binder in the manufacturing operation. This provides a stable mat which can be handled, cut, or fabricated to exact dimensions and can be installed with ease. The binder can be removed by heating to 900ºF for 1 hour, or at 500ºF for 24 hours. Binder content on the Astroquartz mat is between 4% and 5% by weight. Cut sheets of approximately 500 mm x 500 mm (20 in x 20 in) are also available with an area of approximately 2.8 ft per sheet.

Astroquartz ® II RovingAstroquartz II ® roving is made from continuous filaments ofpure fused silica nine microns in diameter. Fiber compositionis 99.99% SiO (silica) exclusive of binder. Standard 20 end roving equivalent to 20 ends of 150 1/0 contains 4800 nine micron diameter filaments. The fiber density is 2.2 g/cm . Astroquartz II ® roving has a fiber tensile strength of 0.5 MSI*

Property Data** Type End Count• Binder•• Yds/Lb† Strength††552 20 9779/9989 750 65 lbs552 12 9779/9989 1250 40 lbs552 8 9779/9989 1875 25 lbs552 6 9779/9989 2500 20 lbs

* Test Method - ASTM D-234 ** Test Method - ASTM D-578 • +0-1 ••0.3%-0.6% LOI † ±10% †† Tensile, min. avg., uncoated roving

2

22

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44

Astroquartz ® Roving (cont.)Astroquartz II ® roving is available with an end count lessthan 20, please consult JPS for details. Other finishes arealso available.

Standard PackagingInside Diameter..............................................................3 inLength.......................................................................... 11 inTraverse.......................................................................10 inWaywind........................................................................ 3 inWind Direction........................................................ForwardType Build...............................................................StraightMaximum OD..............................................................7 OD

Approximate Net Weight9779 Binder...............................................................2.2 lbs

Astroquartz II ® Sewing ThreadAstroquartz II ® sewing thread is made from high purity, extremely fine, continuous filaments of pure fused silica; capable of extended exposure to 2000ºF. Fiber composition is 99.99% SiO (silica) exclusive of binder. Astroquartz II ® sewing threads are supplied coated with PTFE.

With 9855 Teflon Coating (20±4%) Approx. Breaking Approx.Type Diameter Strength* Yield** (in) Typical (lb) Minimal Uncoated CoatedQ-12 0.014 15 12 3660 2925Q-18 0.017 24 19 2440 1950Q-24 0.022 30 25 1830 1460Q-27 0.024 30 25 - 900

* Test Method - ASTM D-578** ±10% Standard PackagingAstroquartz II ® sewing thread are typically available in 0.5 kg spools. Please contact JPS for price and delivery lead times.

2

45

Astroquartz ® YarnAstroquartz ® yarn is made from extremely fine continuous filaments of 99.99% pure fused silica, exclusive of binder, capable of extended heat exposure to 2000ºF.

Astroquartz ® yarn has more than five times the yarn yield of high silica leached yarn. This results in higher tensile strength and abrasion resistance. With Astroquartz ® high production efficiencies are possible in the production of high temperature flexible insulation.

Astroquartz ® yarn is widely used in the form of braided insulation for thermocouple wire, coaxial cables, space separators, hoop wire, and heating elements

Property Data Approx. Approx. Approx.Type Diameter (in) Breaking ε (lb)* Yield (yd/lb)300 2/0 0.008 3 15000300 2/2 0.012 6 7500300 2/4 0.018 10 3750300 2/8 0.020 24 1875*Test Method - ASTM D-578

Astroquartz ® yarns are available with an amino-silane binder system, compatible with phenolic, epoxy, and some polyimide resins. Heavier or lighter count yarns can also be manufactured. Please consult JPS for price and delivery.

Standard PackagingYarns are available on standard milk bottle packages for plied yarns and double flanged packages for twisted single yarn. Net yarn weights range from a minimum of 1 lb/pkg to a maximum of 2.5 lb/pkg.Fiber CharacteristicsAstroquartz II ®* Astroquartz III ®**Number of Filaments300 1/0 - 120 filaments 125 1/0 - 120 filaments300 2/0 - 240 filaments 125 2/0 - 240 filaments300 2/2 - 480 filaments * Astroquartz II ® filaments are 9 µm in diameter, similar to an ECG filament * Each filament is 9 µm in diameter, equivalent to an ECK filament.

46

Physical Properties of Para-AramidsPara-Aramids - Kevlar ®*, Twaron ®**

Physical PropertiesDensity..................................................................1.44 g/ccEquilibrium Moisture Level, Kevlar 29.........................4.5%Equilibrium Moisture Level, Kevlar 49.........................3.5%

Mechanical PropertiesUTS (room temp).............................................2.9-3.0 GPaElongation at Break.............................................. 2.4-3.6%Young’s Modulus..............................................71-112 GPaShear Modulus.................................................. 26-41 GPaPoisson’s Ratio.......................................................... ....0.36

Thermal PropertiesShrinkage in Water at 212ºF (100ºC)........................<0.1%Shrinkage in Dry Air at 351ºF (177ºC)...................... <0.1%Specific Heat Capacity at 77ºF (25ºC)...........1.420 kJ/kg-KSpecific Heat Capacity at 212ºF (100ºC)........ 2.01 kJ/kg-KSpecific Heat Capacity at 356ºF (180ºC)........ 2.52 kJ/kg-KThermal Conductivity........................................0.04 W/m-KDecomposition Temperature in Air......................800-900ºCRecommended Max Temperature Range for Long Term Use in air..........................149-177ºCHeat of Combustion....................................... 35x10^6 J/kg

* Kevlar ® is a registered trademark of the E.I. DuPont du Nemours

** Twaron ® is a registered trademark of Teijin Twaron USA, Inc.

All values approximate. Actual values may vary, for further info contact JPS

47

Physical Properties of UHMWPEUltra High Molecular Weight Polyethylene - Dyneema ®*, Spectra ®**

Physical PropertiesDensity..................................................................0.97 g/cc

Mechanical PropertiesUTS (Spectra 900).............................................25-30 GPaUTS (Spectra 1000)...........................................35-43 GPaElongation at Break (Spectra 900)........................ 3.6-3.9%Elongation at Break (Spectra 1000)...................... 2.9-3.5%Young’s Modulus (Spectra 900).....................850-920 GPaYoung’s Modulus (Spectra 1000)............... 1170-1580 GPa

Thermal PropertiesMelting Range....................................................144-152ºCDecomposition Temperature in Air.......................... >300ºCAdvised Lowest Temperature................................ No LimitAdvised Long Duration Temperature Limit.................. 70ºCAdvised Short Duration Temperature Limit Non-Constrained Fiber..............................130ºC Constrained Fiber...................................... 145ºCTensile Strength Relative to 23ºC at -60ºC......................................................110% at 23ºC....................................................... 100% at 60ºC......................................................... 80% at 100ºC....................................................... 55%

* Dynnema ® is a registered trademark of Royal DSM N.V.

** Spectra ® is a registered trademark of Honeywell International Corp.

All values approximate. Actual values may vary, for further info contact JPS

48

Advanced Materials ApplicationsBallistics and Protection ProductsJPS manufactures high performance fabrics for use in ballistic resistant applications. High performance fabricsare used extensively in bullet, fragment, and stab resistant body armor for militaries, federal agencies, police, and correctional departments. They are also used in the manufacture of helmets for both military and civilian agencies.

Aerospace and Recreational Composites JPS high performance fabrics are used in a variety ofcomposite applications. Aramids and other high performance fabrics are designed to maximize strength, weight savings, durability, and cost. Applications include aerospace, kayaks, recreational sporting goods, and safety equipment, among others.

Advanced Fabrics NomenclatureHigh performance fibers are typically designated by denier,tex, or decitex (dtex). Each is described below.

DenierThe denier system is used internationally to measure the size of textile filaments and yarns. Denier number indicates the weight in grams of 9,000 meters of filament or filament yarn. For example, if 9,000 meters weighs 100 grams, it is a 100-denier yarn. The smaller the denier number, the finer the yarn.

Denier = dtex X 0.9

Tex and DecitexThe tex system is also applicable to the measurement of filament yarns. It is based on the weight in grams of onekilometer (3,300 feet) of yarn. Decitex (dtex) is defined as ten times tex.

Tex = dtex/10

49

Finishes for Advanced MaterialsA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPS.

Finish Name DescriptionCS-811 Loom state fabricCS-800 Scoured aramid fabrics CS-802 Scoured UHMWPE fabrics

CS-892 Water repellent finish for Spectra and Dyneema fabrics

CS-898 Traditional water repellent finish for Kevlar fabrics

CS-899 Traditional water repellent finish for Twaron fabrics

LCS Laminated Composite SubstrateML Micro-Laminate WRT Water Repellent Treated

CS-6000 Engineered aramid water repellent treatment for improved performance

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) (m

ils)

(m

m)

W

arp

Fill

349

350

351

5351

352

5352

353

5353

354

5354

357

372

383

5383

384

4H S

atin

Plai

nPl

ain

Plai

nPl

ain

Plai

n4H

Sat

in4H

Sat

inPl

ain

Plai

nPl

ain

4x4

Twill

5H S

atin

5H S

atin

Bask

et 4

x4

41 34 22 22 17 17 17 17 13 13 11 72 16 16 28

40 34 22 22 17 17 17 17 13 13 17 72 16 16 28

Kev

lar 4

9 19

5d K

evla

r 49

195d

Kev

lar 4

9 38

0d Tw

aron

105

5 40

5dt

Kev

lar 4

9 11

40d

Twar

on 2

200

1270

dt K

evla

r 49

1140

d Tw

aron

220

0 12

70dt

Kev

lar 4

9 14

20d

Twar

on 2

200

1580

dt K

evla

r 49

1420

d K

evla

r 49

195d

Kev

lar 4

9 21

60d

Twar

on 2

200

2420

dt K

evla

r 49

1420

d

Kev

lar 4

9 19

5d K

evla

r 49

195d

Kev

lar 4

9 38

0d Tw

aron

105

5 40

5dt

Kev

lar 4

9 11

40d

Twar

on 2

200

1270

dt K

evla

r 49

1140

d Tw

aron

220

0 12

70dt

Kev

lar 4

9 14

20d

Twar

on 2

200

1580

dt K

evla

r 49

1420

d K

evla

r 49

195d

Kev

lar 4

9 21

60d

Twar

on 2

200

2420

dt K

evla

r 49

1420

d

2.0

1.8

2.2

2.2

5.2

5.2

5.2

5.2

4.9

4.9

5.2

3.8

9.1

9.1

10.7

68 61 75 75 176

176

176

176

166

166

176

129

309

309

363

4.0

3.9

4.8

4.6

9.8

10.7

9.3

9.7

9.8

10.0

10.0

7.0

13.0

13.0

19.0

0.10

0.10

0.12

0.12

0.25

0.27

0.24

0.25

0.25

0.25

0.25

0.18

0.33

0.33

0.48

230

200

300

300

750

800

660

750

650

550

410

520

920

920

1360

230

200

300

300

700

800

650

750

650

550

700

550

970

970

1300

X X X X X

120

220

220

281

281

285

285

500

500

540

900

900

1050

Aram

id F

abric

s

The

phys

ical

pro

perti

es li

sted

are

for g

reig

e (u

ntre

ated

) fab

rics.

Act

ual v

alue

s m

ay v

ary.

For a

dditi

onal

info

rmat

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

51

Sty

le #

Wea

ve

C

ount

War

p

F

ill

Wei

ght

Th

ickn

ess

Stre

ngth

(lbf/i

n)

JPS

A

MS

Com

mon

W

arp

Fi

ll

Y

arn

Yarn

(osy

)

(gsm

) (m

ils)

(m

m)

W

arp

Fill

5384

386

5386

388

5388

710

712

5712

713

5713

715

716

717

718

719

1050

1350

1350

1033

Bask

et 8

x8Pl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

n2x

2 Tw

ill2x

2 Tw

ill

28 27 27 40 40 24 12 12 31 31 28 31 34 34 38

28 22 22 40 40 24 12 12 31 31 28 31 34 34 38

Twar

on 2

200

1580

dt K

evla

r 49

2160

d Tw

aron

220

0 24

20dt

Kev

lar 4

9 14

20d

Tw

aron

220

0 15

80dt

Kev

lar 2

9 15

00d

Kev

lar 2

9 30

00d

Twar

on 1

000

3360

dt

Kev

lar 2

9 10

00d

Twar

on 2

040

1100

dt K

evle

r KM

2+ 4

00d

Kev

ler K

M2+

400

d K

evle

r KM

2+ 4

00d

Kev

ler K

M2+

400

d K

evle

r KM

2+ 4

00d

Twar

on 2

200

1580

dt K

evla

r 49

2160

d Tw

aron

220

0 24

20dt

Kev

lar 4

9 14

20d

Tw

aron

220

0 15

80d

Kev

lar 2

9 15

00d

Kev

lar 2

9 30

00d

Twar

on 1

000

3360

dt K

evla

r 29

1000

d Tw

aron

204

0 11

00dt

Kev

ler K

M2+

400

d K

evle

r KM

2+ 4

00d

Kev

ler K

M2+

400

d K

evle

r KM

2+ 4

00d

Kev

ler K

M2+

400

d

10.7

13.9

13.9

15.5

15.5

9.7

9.1

9.1

8.2

8.2

2.9

3.2

3.6

3.6

4.0

363

471

471

526

526

324

309

309

278

278

99 109

122

122

136

19.0

26.4

26.4

27.6

26.9

19.4

16.5

16.5

16.8

16.3

5.3

5.7

6.3

5.6

6.2

0.48

0.67

0.67

0.70

0.68

0.49

0.42

0.42

0.43

0.41

0.13

0.14

0.16

0.14

0.16

1360

1800

1820

1900

1830

1100

1200

1200

780

900

510

560

580

620

710

1360

1500

1500

1700

1790

1200

1200

1200

1000

900

530

550

630

600

710

1050

1350

1350

1033

1033

Aram

id F

abric

s

The

phys

ical

pro

perti

es li

sted

are

for g

reig

e (u

ntre

ated

) fab

rics.

Act

ual v

alue

s m

ay v

ary.

For a

dditi

onal

info

rmat

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

52

Sty

le #

Wea

ve

C

ount

War

p

F

ill

Wei

ght

Th

ickn

ess

Stre

ngth

(lbf/i

n)

JPS

A

MS

Com

mon

W

arp

Fi

ll

Y

arn

Yarn

(osy

)

(gsm

) (m

ils)

(m

m)

W

arp

Fill

5719

720

722

724

5724

725

5726

728

727

5728

729

730

5731

735

736

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nBa

sket

2x2

Bask

et 2

x2

19.5 20 22 24 24 27 26 17 26 17 17 22 31 35 36

19.5 20 22 24 24 27 26 17 26 17 17 22 31 35 36

Twar

on 2

040

930d

t K

evla

r 129

142

0d K

evla

r 129

142

0d K

evla

r KM

2+ 1

000d

Twar

on 2

040

1100

dt K

evle

r KM

2+ 5

00d

Tw

aron

204

0 93

0dt

Kev

lar K

29 1

500d

Kev

lar 1

29 1

000d

Twar

on 2

040

1680

dt K

evla

r 129

142

0d K

evla

r 29

1000

d T

war

on 2

040

1100

dt K

evla

r 29

1500

d K

evla

r 129

142

0d

4.3

7.6

8.5

6.2

6.2

3.5

5.8

6.6

6.7

6.9

6.6

5.6

8.1

14.1

14.1

146

259

289

210

210

119

200

224

227

234

224

190

275

478

478

7.5

13.8

15.8

11.4

11.0

6.3

10.1

12.7

12.3

12.1

12.8

11.6

16.1

25.4

26.3

0.19

0.35

0.40

0.29

0.28

0.16

0.26

0.32

0.31

0.31

0.33

0.29

0.41

0.65

0.67

600

1000

600

760

760

580

900

900

910

780

900

800

760

1700

1950

600

1000

900

780

780

600

900

900

980

800

900

800

770

1800

2000

X X X

Twar

on 2

040

930d

t K

evla

r 129

142

0d K

evla

r 129

142

0d K

evla

r KM

2+ 1

000d

Twar

on 2

040

1100

dt K

evle

r KM

2+ 5

00d

Tw

aron

204

0 93

0dt

Kev

lar K

29 1

500d

Kev

lar 1

29 1

000d

Twar

on 2

040

1680

dt K

evla

r 129

142

0d K

evla

r 29

1000

d T

war

on 2

040

1100

dt K

evla

r 29

1500

d K

evla

r 129

142

0d

Aram

id F

abric

s

The

phys

ical

pro

perti

es li

sted

are

for g

reig

e (u

ntre

ated

) fab

rics.

Act

ual v

alue

s m

ay v

ary.

For a

dditi

onal

info

rmat

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

53

Sty

le #

Wea

ve

C

ount

War

p

F

ill

Wei

ght

Th

ickn

ess

Stre

ngth

(lbf/i

n)

JPS

A

MS

Com

mon

W

arp

Fi

ll

Y

arn

Yarn

(osy

)

(gsm

) (m

ils)

(m

m)

W

arp

Fill

739

740

741

5741

742

743

744

745

5745

746

747

748

749

750

754

Plai

nPl

ain

Plai

nPl

ain

Plai

nTw

ill 4x

42x

2 Tw

illlPl

ain

Plai

n4H

Sat

inPl

ain

Bask

et 8

x8Pl

ain

2x2

Twill

Bask

et 2

x2

39 40 11 11 31 40 31 17 17 31 10 48 24 24 21

36 40 11 11 31 40 31 17 17 31 10 48 24 24 21

Kev

lar 2

9 15

00d

Kev

lar 2

9 20

0d K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

Kev

lar K

M2+

600

d K

evla

r 29

3000

d K

evla

r KM

2+ 6

00d

Kev

lar 2

9 30

00d

Twar

on 1

000

3000

dt

Kev

lar K

M2+

600

d K

evla

r 29

3000

d K

evla

r 29

1500

d K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

600

dKe

vlar

29

3000

d

Kev

lar 2

9 15

00d

Kev

lar 2

9 20

0d K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

Kev

lar K

M2+

600

d K

evla

r 29

3000

d K

evla

r KM

2+ 6

00d

Kev

lar 2

9 30

00d

Twar

on 1

000

3000

dt K

evla

r KM

2+ 6

00d

Kev

lar 2

9 30

00d

Kev

lar 2

9 15

00d

Kev

lar K

M2+

600

d K

evla

r KM

2+ 6

00d

Kevl

ar 2

9 30

00d

15.2

2.1

8.5

8.5

4.9

16.5

4.9

13.3

13.4

4.8

6.5

18.8

3.8

3.8

16.5

517

71 288

288

167

559

167

451

454

163

220

637

129

129

559

25.3

5.2

16.1

15.0

8.0

29.0

8.5

25.3

24.2

8.5

12.0

32.1

6.8

6.9

29.0

0.64

0.13

0.41

0.38

0.20

0.74

0.21

0.64

0.61

0.22

0.30

0.82

0.18

0.18

0.74

2000

340

1100

1100

810

3200

690

1200

1700

690

900

2200

650

720

2000

1800

330

1150

1150

830

3200

710

700

1800

710

1000

2300

720

680

2000

X X

Aram

id F

abric

s

The

phys

ical

pro

perti

es li

sted

are

for g

reig

e (u

ntre

ated

) fab

rics.

Act

ual v

alue

s m

ay v

ary.

For a

dditi

onal

info

rmat

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

54

Sty

le #

Wea

ve

C

ount

War

p

F

ill

Wei

ght

Th

ickn

ess

Stre

ngth

(lbf/i

n)

JPS

A

MS

Com

mon

W

arp

Fi

ll

Y

arn

Yarn

(osy

)

(gsm

) (m

ils)

(m

m)

W

arp

Fill

5754

755

5755

759

760

764

5704

766

767

768

5768

770

772

5772

5761

Bask

et 2

x2Ba

sket

4x4

Bask

et 4

x4Ba

sket

4x4

Bask

et 2

x2Pl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

n

21 21 21 24 30 31 31 34 28 28 28 31 24 28 26

21 21 21 24 30 31 31 34 28 28 28 31 24 28 26

Twar

on 1

000

3360

dt K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

Kev

lar 2

9 30

00d

Kev

lar 2

9 14

20d

Kev

lar K

M2+

850

d Tw

aron

204

0 93

0dt

Kev

lar K

M2+

600

d K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

500

d Tw

aron

204

0 55

0dt

Kev

lar K

M2+

600

d K

evla

r KM

2 10

00d

Twar

on 2

040

550d

t Tw

aron

204

0 11

00dt

Tw

aron

100

0 33

60dt

Kev

lar 2

9 30

00d

Twar

on 1

000

3360

dt K

evla

r 29

3000

d K

evla

r 29

1420

d K

evla

r KM

2+ 8

50d

Twar

on 2

040

930d

t K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

600

d K

evla

r KM

2+ 5

00d

Twar

on 2

040

550d

t K

evla

r KM

2+ 6

00d

Kev

lar K

M2

1000

d Tw

aron

204

0 55

0dt

Twar

on 2

040

1100

dt

16.2

16.3

16.2

18.0

11.8

6.8

6.8

5.4

4.4

3.6

3.6

4.8

6.2

3.6

6.7

549

554

549

610

400

231

231

184

150

122

122

163

210

122

227

30.0

27.9

30.0

30.0

21.1

13.9

13.8

9.8

7.8

6.5

6.5

8.6

11.0

6.6

11.0

0.76

0.71

0.76

0.76

0.54

0.35

0.35

0.25

0.20

0.17

0.17

0.22

0.28

0.17

0.28

2000

2000

2000

2300

850

850

900

800

550

500

500

700

760

500

760

2000

2000

2000

2000

600

1100

950

800

570

550

500

800

780

550

780

X X X X

Aram

id F

abric

s

The

phys

ical

pro

perti

es li

sted

are

for g

reig

e (u

ntre

ated

) fab

rics.

Act

ual v

alue

s m

ay v

ary.

For a

dditi

onal

info

rmat

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

55

Sty

le #

Wea

ve

C

ount

War

p

F

ill

Wei

ght

Th

ickn

ess

Stre

ngth

(lbf/i

n)

JPS

A

MS

Com

mon

W

arp

Fi

ll

Y

arn

Yarn

(osy

)

(gsm

) (m

ils)

(m

m)

W

arp

Fill

5774

775

777

779

785

787

790

794

796

797

798

4033

4039

5930

5931

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nTw

ill 2x

2Pl

ain

Bask

et 2

x2Pl

ain

Plai

nPl

ain

Plai

nPl

ain

27 31 32 70 20 23 22 26 26 34 28 23 29 27 31

27 31 32 70 20 23 22 26 26 34 28 23 29 27 31

Twar

on 2

040

500d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 4

00d

Kev

lar 1

59 2

00d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 8

50d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 8

40d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

400

d K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

600

d T

war

on 2

040

930d

t Tw

aron

204

0 93

0dt

Twar

on 2

040

500d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 4

00d

Kev

lar 1

59 2

00d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 8

50d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 8

40d

Kev

lar K

M2+

850

d K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

400

d K

evla

r KM

2+ 6

00d

Kev

lar K

M2+

600

d Tw

aron

204

0 93

0dt

Twar

on 2

040

930d

t

3.6

6.8

3.2

3.7

4.4

5.1

4.3

5.7

5.8

5.3

2.9

3.5

4.5

5.8

7.0

122

231

108

122

150

173

146

194

200

180

98 119

153

197

237

6.5

11.8

6.2

7.6

7.6

8.7

7.5

9.6

10.2

8.9

5.6

6.9

8.4

10.5

12.0

0.17

0.30

0.16

0.19

0.19

0.22

0.19

0.24

0.26

0.23

0.14

0.18

0.21

0.27

0.31

580

880

450

350

700

800

600

850

850

750

800

600

700

850

900

610

950

450

350

700

800

600

950

950

850

600

600

700

950

950

X X X X X X X X X

Aram

id F

abric

s

The

phys

ical

pro

perti

es li

sted

are

for g

reig

e (u

ntre

ated

) fab

rics.

Act

ual v

alue

s m

ay v

ary.

For a

dditi

onal

info

rmat

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(864

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(864

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(864

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64

Carbon FabricsJPS Composite Materials now offers a full line of carbon fabrics, available with a wide variety of yarn types and weights. We have invested in the production of carbonfabrics using the latest new weaving technologies. Withthe addition of our new carbon fabrics division JPS offers the most complete lineup of composite reinforcement fabrics in the industry.

We offer a variety of PAN based carbon fabrics utilizing 3k, 4k, 6k, and 12k carbon fibers. Our carbon fabrics are manufactured in a dedicated, FOD controlled, state-of-the-art facility located on our Statesville, NC campus.

JPS carbon fabric can be used for a wide variety ofapplications, including and primary and secondary aerospace structures, for high performance and recreational composites, as well as in ducting, tooling, and cosmetic applications.

We invite you to consider using carbon fabrics from JPS for your application. See first hand why we are considered the leader when it comes to high performance, precision engineered composite reinforcement materials.

For more information about our carbon fabrics, or to tailor a fabric to suit your application, please contact us at:

1-800-431-11101-800-288-0577(864) 260-6581 Fax

For further information, write to JPS Composite MaterialsPO Box 2627, Anderson, SC, 29622dhudgens@jpscm.com

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d K

evla

r ® K

M2+

500

d K

evla

r ® K

M2+

600

d K

evla

r ® K

M2+

850

d S

pect

ra ®

900

650

d S

pect

ra ®

100

0 37

5d S

pect

ra ®

200

0 19

5dTw

aron

® 1

000

Twar

on ®

200

0Tw

aron

® H

M

0.09

50.

090

0.08

00.

052

0.05

20.

052

0.05

20.

052

0.05

20.

035

0.03

50.

035

0.05

20.

052

0.05

2

500

665

870

424

424

520

525

525

512

348

410

465

507

479

507

10.5

12.5

10.0

15.8

10.9

13.6

10.8

13.6

11.8

11.4

14.9

16.4

9.4

12.9

14.7

4.0

5.5 - 2.5

3.4

3.8

3.8

3.8

3.8

3.6

3.1

2.9

3.7

3.3

2.1

5.28

7.42 -

8.15

8.15

10.0

010

.10

10.1

09.

859.

9311

.70

13.2

79.

749.

219.

69

1.11

1.40 -

3.04

2.10

2.61

2.08

2.61

2.27

3.25

4.25

4.68

1.81

2.50

2.85

3.00

0.90

0.54

-1.5

0-1

.22

-1.2

2-1

.22

-1.2

2-1

.22

- - --1

.22

-1.2

2-1

.33

1346

1562

3092

842

842

842

842

842

842

302

302

302

842

842

842

Tech

nica

l Ref

eren

ces

- Eng

lish

66

Stra

in

Spe

cific

Spe

cific

C

oeffi

cien

t

Tens

ile

T

ensi

le

to

Te

nsile

Te

nsile

of T

herm

al

Dec

ompo

sitio

n

D

ensi

ty

Stre

ngth

M

odul

us F

ailu

re

Stre

ngth

Mod

ulus

E

xpan

sion

Tem

pera

ture

F

iber

(g/c

m )

(

GPa

)

(G

Pa)

(%

)

(10

cm

)

(10

cm

)

(10

/ºC

)

(º

C)

86

3-6

E-gl

ass

S-2

® G

lass

Astro

quar

tz ®

Kev

lar ®

49,

142

0d K

evla

r ® 2

9 15

00d

Kev

lar ®

KM

2+ 4

00d

Kev

lar ®

KM

2+ 5

00d

Kev

lar ®

KM

2+ 6

00d

Kev

lar ®

KM

2+ 8

50d

Spe

ctra

® 9

00 6

50d

Spe

ctra

® 1

000

375d

Spe

ctra

® 2

000

195d

Twar

on ®

100

0Tw

aron

® 2

000

Twar

on ®

220

0

2.50

2.48

2.20

1.44

1.44

1.44

1.44

1.44

1.44

0.97

0.97

0.97

1.44

1.44

1.45

2.6

4.8

6.0

2.9

2.9

3.3

3.4

3.4

3.4

2.4

2.8

3.2

3.5

3.3

3.5

72 85 72 109

75 94 75 94 81 79 103

113

65 90 103

4.0

5.5 - 2.5

3.3

3.8

3.8

3.8

3.8

3.6

3.1

2.9

3.7

3.3

2.1

13.4

218

.86

-20

.71

29.7

123

.39

24.2

724

.60

24.2

725

.23

29.7

233

.71

24.7

623

.39

24.5

9

2.82

3.55 -

7.72

5.32

6.64

5.27

7.52

5.76

8.26

10.8

011

.89

4.59

6.35

7.23

1.60

0.48

0.54

-2.7

0-2

.20

-2.2

0-2

.20

-2.2

0-2

.20

- - --2

.20

-2.2

0-2

.40

730

850

1700

450

450

450

450

450

450

150

150

150

450

450

450

Tech

nica

l Ref

eren

ces

- Met

ric

67

Selected Conversions and FormulaeUS to SI SI to US

1 oz/yd = 33.91 g/m 1 g/m = 0.0295 oz/yd

1 oz = 28.35 g 1 g = 0.035 oz1 lb = 16 oz

1 lb = 0.454 kg 1 kg = 2.205 lb

1 N = 0.102 kgf 1 kgf = 9.81 N1 lbf = 4.45 N 1 psi = 6894.76 Pa 1 ksi = 6.89 MPa 1 MPa = 1 N/mm 1GPa = 1000 MPa

1 denier = 0.111 Tex 1 Tex = 9 denier 1 Tex = 496,052 yds/lbs

ºF = (ºC)*(9/5)+32 ºC = (ºF-32)*(5/9)

1 in = 25.4 mm = 2.54 cm 1 cm = 0.39 in

1 lb/ft = 4.88 kg/m 1 kg/m = 0.205 lb/ft1 lb/ft = 16.02 kg/m 1 kg/m = 0.062 lb/ft

1 yd = 0.91 m 1 m = 1.09 yd

1 ft = 0.3048 m 1 m = 3.281 ft

1 w.m .k = 0.86 kcal.m .h .k = 6.9 btu.in/(ft.hr.ºF)

Metric Conversion ChartFabric US Factor MetricLength yd x 0.914 = mWidth in x 2.540 = cmWeight oz/yd x 33.906 = g/mBreaking Strength lb/in x 1.7513 = N/cmThickness in x 25.400 = mmMullen Burst lb/in x 0.007 = MPaAir Permeability cfm x 0.508 = cm/cmArea yd x 0.8361 = m

2 2 2 2

2

-1 -1 -1 -1 -1

2 23 3

2 23 3

2 2

2

2 22

68

Notes

69A Handy & Harman Company

JPS Composite Materials2200 South Murray Avenue

P.O. Box 2627Anderson, SC, 29622

(864) 224-3506(800) 431-1110 Toll Free(800) 288-0577 Toll Free

(864) 260-6581 Fax

Notes

A Handy & Harman Company

JPS Composite Materials2200 South Murray Avenue

P.O. Box 2627Anderson, SC, 29622

(864) 224-3506(800) 431-1110 Toll Free(800) 288-0577 Toll Free

(864) 260-6581 Fax70