Jps Databook

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description

Jps Databook

Transcript of Jps Databook

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(864) 260-6581 Fax

Table of ContentsCompany............................................................................ 1Locations........................................................................... 1Conditions of Sales........................................................... 2Parameters for Fabric Selection.........................................3Fiberglass Yarn Nomenclature........................................... 4Glass Composition............................................................. 4Basic Glass Yarn Strands...................................................6Design Consideration for Glass Fabric Selection...............6Manufacturing Process...................................................... 7Weave Patterns..................................................................9Specifications & Standards.............................................. 13

FIBERGLASS PRODUCTS............................................. 15Physical Properties of E-glass......................................... 15Physical Properties of S-2 ® Glass..................................16Fiberglass Fabric Applications......................................... 17Fiberglass Fabric Finishes............................................... 18Finishes for EIFS............................................................. 19Finishes for Filtration Fabrics.......................................... 20

FIBERGLASS FABRIC CONSTRUCTIONS.................... 21Fiberglass Fabric Weight Index........................................ 34Fiberglass Fabric Thickness Index.................................. 37Filtration Fabrics.............................................................. 40Filtration Finished Fabrics............................................... 41EIFS Mesh Fabrics.......................................................... 42Insulation GlasTex Fabrics.............................................. 43

ASTROQUARTZ ® PRODUCTS..................................... 44Physical Properties of Astroquartz II ®............................ 44Astroquartz ® Applications and Design Considerations.. 45Astroquartz ® II & III Fabric Finishes............................... 46Astroquartz II ® Chopped Fiber....................................... 47

ASTROQUARTZ ® II & III FABRICS............................... 48Astroquartz ® Mat Style No. 550..................................... 49Astroquartz ® II Roving................................................... 49Astroquartz ® II Sewing Thread....................................... 50Astroquartz ® II Yarn........................................................ 51

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ADVANCED MATERIALS PRODUCTS........................ 52Physical Properties of Aramid Fibers............................ 52Physical Properties of Selected Advanced Performance Fibers...................................... 52Advanced Materials Applications................................... 53Advanced Materials Fiber Nomenclature...................... 53Finishes for Advanced Materials................................... 54

Aramid Fabric Constructions......................................... 55Aramid Fabric Weight Index.......................................... 62Aramid Fabric Thickness Index..................................... 64

Spectra Fabrics............................................................. 66

Technical References - English..................................... 67

Technical References - Metric....................................... 68Selected Conversions & Formulae................................ 69Notes............................................................................. 70

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Company

JPS Composite Materials, a wholly owned subsidiary of JPS Industries Inc., is the world’s leading manufacturer of high strength fiberglass, Astroquartz ®, and aramid fabrics andreinforcements. Our materials are used extensively in reinforcing and insulating applications in fields including electronics, aerospace, marine, surf, advanced composites,ballistics, architecture, construction, and sporting goods. Our materials are readily adaptable to unlimited designs.

Direct customer access to customer service and management personnel:

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

For further information, write to JPS Composite MaterialsPO Box 2627, Anderson, SC, 29622

LocationsAnderson, South CarolinaCorporate HeadquartersTechnical Development CenterAdvanced, Aerospace Composite, Astroquartz ®, and Ballistic Fabrics

Slater, South CarolinaTechnical Development CenterAstroquartz ®, Advanced, Aerospace Composite, Boat, Tooling, Coating, EIFS, Building Products and General Industrial Fabrics

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

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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 composite reinforcements (yarn type, fabric construction, widths, finishes and other facts), the technical data and other information contained on these pages is intended as a general guide and is subject to change without notification unless specifically prohibited by specific purchase specifications.

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Parameters for Fabric SelectionIn selecting a woven fabric for industrial applications, a number of design parameters may be considered, these are broken down into four basic variables: Yarn Weight, Thread Count, Weave Pattern, and Fabric Finish. The wide range of yarn weights and counts available provide the base for fabric design.

Yarn weight, combined with thread count (the number of warp ends (lengthwise) and filling picks (width wise) per inch) determines the strength, weight and thickness of the fabric.

Basic weaving concepts are utilized in the manufacture of high performance fibers and fabrics, such as glass and aramid. The technology, however, is advanced to incorporate specialized precision equipment to meet the exacting demands of modern applications. For composite applications there are sixbasic fabric patterns: Plain, Basket, Leno, Four Harness Satin, Eight Harness Satin, and Twill.

YarnFiberglass is glass in fiber form. All forms of glass fibers begin with similar manufacturing processes. The various ingredients are mixed in a batch to make a specific formulation and then high temperatures convert the mix into molten glass. Continuous filaments are attenuated (drawn or pulled rapidly) from the molten glass through a precision multihole spinneret. A yarn strand is produced by combining many individual continuous filaments (from 51 to 1632) Immediately after drawing filaments are coated with an organic binder to protect them from damage during handling, processing and weaving.

FormulationsGlass fibers are made from different formulations: “E” being the most common all-purpose glass, while “S”, “T”, “L” and others are made for special applications. Astroquartz ® II and III quartz fiber products are the purest form of silica. The chemical composition of the most common glass formulations is shown on the next page.

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COMPOSITION OF TYPICAL GLASSES (%) by weight

“E” “S”, “T” Ingredient Glass Glass “Astroquartz ® 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 types which are produced. The nomenclature is used for filament and yarn identification consists of two basic parts - one alphabetical, todescribe the composition and construction, and the other numerical, to describe the weight and number of yarnstwisted and plied together.

A typical example and the of its letters and numerals follow:

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 Plied Filament Yardage/Lb Together (in Hundreds)

As shown, the letters describe the basic strand by composition, type and diameter. Numbers identify strand weight and yarn construction. The above description wouldbe for ECG 150 1/2 yarn, or more simple G-150 1/2, used instyle 1581 fabric. The S-glass equivalent used in style 6781 fabrice would be SCG 150 1/2, where “S” denotes S-glass.

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The strand count is the first series of numbers following the letters and indicates approximate yardage per pound, in hundreds (i.e. to compute the number of yards in a pound of strand, multiply the strand count by 100).

The second series of numbers designates the number of plies in continuous filament yarns.

The first digit 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, 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, 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 strand

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

Approximate yards per pound of fabricated yarn can be computed by dividing the strand count, multiplied by 100, by the number of strands.

Therefore: 150 x 100 1 x 2The results of this computation must always be considered approximate because yards per pound are reduced slightly in the twisting and plying operations.

= 7500 yds/lb for fabricated yarn

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DESCRIPTION OF CONTINUOUS FILAMENT GLASS FIBERS Strand Nominal Filament Count Filament Number Designation (x100=yd/lb) Dia. (in) of Filaments

B 150 0.00015 1224

C 150 0.00015 816

D 1800 0.00023 51 900 0.00023 102 450 0.00023 204 225 0.00023 408 DE 150 0.00025 408 75 0.00025 816 50 0.00025 1632 37 0.00025 1632

E 225 0.00029 204

G 150 0.00036 204 75 0.00036 408 37 0.00036 816

H 25 0.00043 816

K 75 0.00051 204 37 0.00051 408 25 0.00051 608 18 0.00051 816

DESIGN CONSIDERATIONS FOR GLASS FABRIC SELECTIONThere are five basic design variables toconsider when choosing fabric for industrial use:

ThicknessGlass fabrics are available in thicknesses ranging from ~0.0010” to ~0.060”.

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WeightThe weight range begins at less than 1 ounce per square yard to over 50 ounces per square yard.

Yarn SizeYarn size determines the weight and thickness of the fabric. For specific applications, one yarn may be selected over another to the advantage of the fabric’s physical and mechnical performance characteristics.

ConstructionThis is determined by the number of warp yarns (machine direction) and fill yarns (cross-machine direction) per inch of the fabric and by the weave pattern.

FinishMost industrial applications require that fabric be used with acoating material. For compatibility with resins coatings, an organic finish or after treatment is often applied to the fabric.

YARN CONSTRUCTION

Twisting/PlyingThis process serves to control the yarn strength, diameter, weight, and flexibility. Filaments are twisted to a predetermined specification, and the twisted threads are then combined or plied to balance and avoid any stresses in the yarn that may cause processing difficulties. Many glass fabrics are woven from single yarns as received from the yarn producers.

WarpingWarping, shown in the drawing, is essentially the laying of the yarns in parallel order. A specified number of threads 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 threads per inch required in the fabric specification.

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The combination of section beams occurs during the slashing process to create the warp, or loom, beam. This entire system of parallel threads is wound on one loom beam to become the “warp”, or lengthwise system of threads in the fabric.

SlashingSlashing is employed when non twisted yarn is used. Warp sizing is applied to the yarns to facilitate handling and to provide protection during the weaving process. This operation involves (1) sizing single-fiberglass warp yarnswith a specially compounded chemical formulation, (2) drying the yarns, and (3) winding the desired number of ends on the loom beam through the combination of section beams.

EnteringThe entering operation prepares warp yarn for weaving. In this process, the warp yarns are threaded from the loom beam through the headle eyes on the proper harnesses to achieve the desired pattern in the fabric. The warp yarn is then drawn through a reed to establish the warp thread count. The reed is also used to place the filling yarns in their proper position.

WeavingWeaving consists of interlacing a series of filling yarns with a series of warp yarns at right angles. The filling yarns are inserted by an air jet, rapier or shuttle that traverses the yarns from one side of the warp to the other, interlacing the two systems of threads, “warp” and “filling”, in a prearranged weave plan.

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FinishingCoupling agents are applied to the fabric during finishing.The coupling, or finishing, agents act to provide optimum adhesion between the reinforcement fabric and the polymermatrix. Ballistic fabrics may undergo scouring and water repellent treatment in the finishing stage.

Weave PatternsThe matching of yarn, weave and finish for a particular requirement is an exacting science. Because fiberglass fabrics are highly engineered, the right combination of fabric weight, thickness and construction is essential in selecting the proper fabric for a particular application.

Selecting the right reinforcement fabric for any requirement can simplified by calling our technicians, design engineers and technical representatives. Their specialized experiencecan aid in selecting a reinforcement fabric suited to your requirements.

The weaving of reinforcement fabrics is a highly complex function that combines the latest in modern machine technology with the art of weaving, which is as old ascivilization. All standard fabric weaves can be produced withfiberglass, aramid, Astroquartz ®, polymer yarns.

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Plain Weave

The plain weave consists of yarns interlaced in an alternating fashion, one over and one under every other yarn. The plain weave provides good fabric stability.

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.

Leno

The leno weave is used where relatively low numbers of yarns are involved. The leno weave locks the yarns in place by crossing two or more warp threads over each other and interlacing with one or more fill threads. Light weight membrane applications such as EIFS use the leno weave.

Four-Harness Satin (Crowfoot)

The four-harness satin weave is more pliable than the plain weave and is easier to conform to curved surfaces typical inreinforced plastics. In this weave pattern there is a three byone interlacing, where a fill yarn floats over three warp yarns and under one.

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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 at least two consecutive picks, permitting more yarns per unit area.

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Specifications and StandardsJPSCM 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 - Covers basic forms of finished fiberglass fabrics.

AMS-3846 - Covers quartz in woven fabric form.

AMS-3902 - Covers cloth woven from continuous multifilament aramid yarn.

AMS-C-9084 - Covers the requirements for woven, cleaned, and finished glass fabrics used in composite applications.

ASTM-D-579 - Standard specifications for testing greige statewoven glass fabrics.

ASTM-D-1668 - Covers open mesh woven glass fabrics used for membrane waterproofing and built up roofing.

ASTM-D-3659 - Covers flame spread for self extinguishing EIFS finishes.

ASTM-D-4029 - Standard specifications for E-glass fabrics for reinforcement use.

ASTM-E-2098 - Covers Alkali resistance for EIFS materials.

BMS 9-3 - Boeing Commercial Airplane Company’s requirements for E-glass fabrics.

IPC-4412 - Covers woven glass fabrics for use in printed circuit boards.

MIL-C-20079 - Covers glass fabric used as lagging material over thermal insulation and for hull insulation board.

MIL-C-22787 - Covers vinyl coated base glass fabrics.

MIL-DTL-44050 - Detailed specifications for aramid cloth for use in ballistic protecion.

MIL-DTL-46593 - Projectile specifcitations for armor testing.

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MIL-DTL-62474 - Covers aramid fabric for use in composite armor systems.

MIL-PRF-64154 - Covers glass fabric for use in composite armor systems.

MIL-R-7575 - Covers glass fabric used in polyester laminates.

MIL-R-9300 - Covers glass fabric for use in epoxy laminates.

MIL-S-662 - V-50 ballistic test for armor applications.

MIL-Y-1140 - Covers untreated glass yarns and fabrics.

FIBERGLASS PRODUCTS

Physical Properties of E-glass Fiber

Approximate Chemistry*SiO .............................................................................52-60%CaO............................................................................. 16-25%Al O ...........................................................................12-16%BaO................................................................................8-13%MgO................................................................................. 0-6%NaO ............................................................................... 0-1%KO ..................................................................................0-1%

Physical Properties*Density...............................................................2.54-2.60 g/ccRefractive Index................................................ 1.558 to 1.562

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 (20ºC).................................................... 4.0-5.0 µm/m-ºCCTE (30ºC to 250ºC)..................................... 4.5-5.5 µm/m-ºCSpecific Heat Capacity................................... 0.78-0.82 J/g-ºCThermal Conductivity.................................... 1.28-1.32 W/m-KSoftening Point............................................................≤ 845ºC

Electrical Properties*Dk @ 1 MHz................................................................. 6.3-6.6Df @ 1 MHz...................................................... 0.0023-0.0027Electrical Resistivity......................................3.5-4.0e+12Ω-cmDielectric Strength..................................................10.3kV/mm

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

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

Physical Properties*Density...............................................................2.44-2.48 g/ccRefractive Index................................................ 1.548 to 1.553Mohs Hardness...................................................................6.5

Mechanical Properties*UTS (room temp)..................................................4.8-4.9 GPaBreaking Strain.......................................................... 5.5-6.0%Young’s Modulus.................................................... 85-90 GPaShear Modulus....................................................... 33-37 GPaPoisson’s Ratio............................................................... 0.230

Thermal Properties*CTE (20ºC).................................................... 1.5-1.7 µm/m-ºCSpecific Heat Capacity................................... 0.72-0.75 J/g-ºCThermal Conductivity.................................... 1.44-1.46 W/m-KSoftening Point..........................................................≤ 1055ºC

Electrical Properties*Dk @ 1 MHz................................................................. 5.0-5.4Df @ 1 MHz...................................................... 0.0018-0.0022Electrical Resistivity......................................8.5-9.1e+10Ω-cm

Corrosion Resistance*† (%weight loss, greige fiber)10% H SO ........................................................................5.7Conc. HCl............................................................................1.410% NHO ...........................................................................7.3H O (Distilled).....................................................................1.010% NaOH or 10% KOH...................................................66.0

*All values approximate. Actual values may vary, for further info contact JPSCM† 1 week immersion @ 205ºF

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Fiberglass Fabric ApplicationsFiberglass fabrics are used in a wide range of industrial applications. The high strength, dimensional stability, design flexibility, and electrical properties are some of the characteristics that ensure optimal performance and economy with this highly engineered material.

Coated and Lamination FabricsFiberglass fabrics can be found in window shades, vapor barriers, movie screens, packaging tapes, awnings, protective clothing, gaskets, conveyor belts and countless other products that improve our lives daily.

ConstructionIn architectural applications fiberglass fabrics provide strength and sustainability to the exterior facades of commercial buildings, and reinforcement for commercial roofing systems.

ElectricalFiberglass 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 worlds leading aircraft, automobiles, buildings, bridges, roadways and sporting goods.

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

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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 technicalsupport representative.

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

Caramelized Uncoated PTFE Loom state fabric, size, (210) PVA 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 color

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

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Finish Functionality: Name Primary Secondary Notes S-910 Polyester High clarity for surf S-912 Polyester Epoxy High clarity for surf 933 HTS Polyimide Epoxy, BT High temperature silane S-977 Epoxy Polyester Silane finish A-1100, Phenolic Epoxy Silane finishA-1100S BMS 9-3 Listed

F81 Epoxy, Vinyl Ester, Multifunctional silane, Polyester Urethane excellent wetting

Z-6040 Epoxy Phenolic Common base silane 9464 Uncoated Epoxy Antimony-fee Hull Board9465 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

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

JPSCM EIFS finishes are designed to provide superiorperformance and enhanced workability in residential and commercial EIFS construction applications. Our Flexmesh™finishes feature both superior impact strength for maintenance areas and excellent hand for ease of applicationin intricate detail areas. All Flexmesh™ finishes are self-extinguishing and alkalie resistent, certified to ASTM standards D-3659 and E-2098.

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Flexmesh Performance Name Features

TM

Standardflex High impact strength for high maintenance areas

TM

Duraflex Good “hand” for flat wall work TM

Ultraflex Excellent for detail and high end work TM

Finishes for Filtration FabricsA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.

Finish Performance Name FeaturesAcid Excellent acid resistance and high flexibility at elevated temperatures. Laminatable with PTFE membranes

9892 Tritemp finish - special formula blend of silicone, fluorocarbon and graphite for max high temperature lubricity of glass fabrics

PTFE PTFE finish with excellent chemical resistance and high temperature lubricity. A “soft hand” finish meets the challenges of many dust collection and air pollution control problems

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Rep

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(864

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(864

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Rep

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(864

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Rep

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(864

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Rep

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(864

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Rep

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(864

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(864

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3.08

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3.10

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3.12

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157

159

159

162

163

164

166

167

168

173

173

178

180

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182

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187

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190

190

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6.53

6.60

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7.05

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207

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212

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43

ASTROQUARTZ ® PRODUCTS*Astroquartz ® is a registered trademark of JPS Industries

Astroquartz ® II &Astroquartz III ® PropertiesAstroquartz ®, Astroquartz II ® and Astroquartz III ® are composed of identical raw materials. Through improved manufacturing and handling technologies Astroquartz II ® and Astroquartz III ® represents a stronger, cleaner products with unparalleled quality, standards, and specifications. Such 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 - Astorquartz III ®....................................14µm

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

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

ThermalLinear 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

3

3 3

-62

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44

Physical Properties of Fused Quartz (cont.)

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

Astroquartz ® Applications and Design ConsiderationsAstroquartz ® fabrics offer better solutions to high heat, highstrength problems.

The aerospace industry relies on Astroquartz ® fiber productsmade from pure fused silica (99.99% SiO ) to produce an outstanding reinforcement material for high temperature and ablative space and missile applications. Astroquartz ® products are recommended when low dielectric loss properties are required, such as microwave transmission in radome and antenna applications.

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

ThicknessQuartz and composite fabrics are available in thicknessesranging from 0.003” to 0.027”.

WeightThe weight for Astroquartz ® fabrics range from two to twelveounces per square inch.

ConstructionConstruction determines the number of warp yarns/denier (in themachine direction) and filling yarns/denier (in the cross-machine direction) per inch of the fabric, thereby helping determine thethickness, weight, and drapability, and overall performance of the fabric.

2

45

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

FinishMost industrial applications require that Astroquartz ® fabric be coated with a coupling agent to assist resin wet out and to improve the strength of the fiber to resin interface, therebyaffecting the mechanical performance characteristics of the final part. For finish or after weaving treatment compatibility with specific resins for specific application please contactJPS technical or customer service.

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 JPSCM.

46

Finish Functionality: Name Primary Secondary Notes S-928 Epoxy Epoxy functional silane 933 HTS Polyimide Epoxy, BT High temperature silane S-977 Epoxy Polyester Silane finish 1059 HT/ Polyimide Thermo- Formulated for high2059 HT/ plastic temperature and3059 HT matrices moisture resistance9779 Epoxy Bismaleimide Amino-silane 9827/ Epoxy Polyimide, Recommended for2827/ Bismaleimide electronic and 3827 aerospace applications

9836/ Epoxy Bismaleimide Scoured fabric to2836/ to remove most organic 3836 binder components

Astroquartz ® II & III Fabric Finishes (cont.)

Astroquartz II ® Chopped FiberAstroquartz II ® chopped fiber is made by cutting continuousfilaments of high purity, extremely fine pure quartz fibers to apredetermined length. Fiber composition is 99.99% SiO (silica) exclusive of binder.

Because of their high strength plus excellent ablative, electrical, and high temperature characteristics, Astroquartz IIchopped fibers are used widely in reinforced plastics, moldingcompounds, and as a ceramic reinforcement.

Type 556 Chopped Fiber

Fiber Lengths* Standard Binder Astroquartz II ® from 1/8” to 1” chopped fiber with an aminosilane binder compatible with epoxy, phenolic and some polyimide resins.

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

Standard Packaging1 lb packages packed loosely in clear polyethylene bags.

247

Finish Functionality: Name Primary Secondary Notes

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

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48

2

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 24hours. 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 endroving 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

Astroquartz ® II roving is available with an end count less than 20, please consult your JPS for details. Other finishesare also available.* Test Method - ASTM D-234 ** Test Method - ASTM D-578 • +0-1 ••0.3%-0.6% LOI † ±10% †† Tensile, min. avg., uncoated roving

22

33

2

2

3

49

Astroquartz ® Roving (cont.)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 that iscapable of extended exposure to 2000ºF. Fiber composition is 99.99% SiO (silica) exclusive of binder. Unless otherwisespecified, Astroquartz II ® sewing threads are supplied coatedwith Teflon.

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 - 1030

* Test Method - ASTM D-578** ±10%

2

50

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.

With more than five times the yarn yield of high silica leachedyarn, Astroquartz ® yarn has a higher tensile strength andabrasion resistance. As a result, high production efficienciesare now possible in the production of high temperatureflexible insulation.

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

Property Data Approx. Approx. Approx.Type Diameter (in) Breaking Strain (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 pliedyarns and double flanged packages for twisted single yarn. Net yarn weights range from a minimum of 1 lb/pkg to amaximum 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 E-glass “G” filament* Each filament is 9 µm in diameter, equivalent to an E-glass “K” filament.

51

ADVANCED MATERIALS PRODUCTSPhysical Properties of Aramid FibersAramids - Kevlar ®*, Twaron ®**High StrengthAramid fibers are 43% lighter than E-glass fibers, with adensity of 1.44 g/cc compared to 2.55 g/cc. Aramids are twiceas strong as E-glass, ten times as strong as Aluminum and approach the strength of carbon fiber on a specific tensilestrength basis.

Dimensional StabilityAramids display excellent dimensional stability, with a slightlynegative coefficient of thermal expansion (-2.4 µm/ºC).

Chemical ResistanceAramids show minimal to no embrittlement and strength lossat temperatures as low as -320ºF. Aramids do not melt or combust, but will carbonize at approximately 800ºF.* Kevlar ® is a registered trademark of the E.I. DuPont du Nemours** Twaron ® is a registered trademaerk of Teijin Twaron USA, Inc.

Physical Properties of SelectedAdvanced Performance FibersUltra High Molecular Weight Polyethylene - Spectra ®High StrengthUHMWPE has a density of 0.97 g/cc making it one of thelightest high performance fibers, with a high strength toweight ratio. This fiber can be up to fifteen times as strong as steel.

Chemical ResistanceUHMWPE has excellent resistance to water, acetic acid, hydrochloric acid, nitric acid, ammonium hydroxide, kerosene, toluene, trichloromethane and microorganisms.This fiber is slightly affected by strong base.

Thermal StabilityThe melting point of UHMWPE is 150ºC. The tenacity andmodulus decrease at higher temperatures but increase insub-zero temperatures. They show essentially no embrittlement at temperatures as low as -150ºC.* Spectra ® is a registered trademark of Honeywell International Corp.

52

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

Marine, Tooling, and Recreational ProductsJPS high performance fabrics, exhibiting the properties ofhigh strength and durability, are used in a variety ofapplications ranging from boating to skiing. Applications aredriven by strength, weight durability, clarity, and cost. Applications include kayaks, boats, hydroplanes, safetyequipment, and other sporting goods.

Advanced Materials Fiber 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 sizeof silk and synthetic filaments and yarns. Denier number indicates the weight in grams of 9,000 meters of filament orfilament 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 tentimes tex.

Tex = dtex/10

For example, 840 denier yarn may also be designated as 933 dtex or 93.3 Tex.

53

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

54

Finish Name DescriptionCS-811 Loom state fabricCS-800 Scoured aramid fabrics CS-802 Scorued Spectra or Dyneema fabrics

CS-892 Water repellent finish for Spectra and Dyneema fabrics

CS-898 Water repellent finish for Kevlar fabrics

CS-899 Water repellent finish for Twaron fabrics

LCS Laminated Composite SubstrateML Micro-Laminate WRT Water Repellent Treated

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

290

296

297

310

311

323

324

5324

328

5328

343

345

348

5348

349

350

351

Leno

Leno

Leno

Plai

nR

ip S

top

4H S

atin

Plai

nPl

ain

Plai

nPl

ain

4H S

atin

4H S

atin

8H S

atin

8H S

atin

4H S

atin

Plai

nPl

ain

9.6 12 14 36 36 17 24 24 17 17 100

34 50 50 41 34 22

5 12 14 36 36 17 24 24 17 17 20 34 50 50 40 34 22

Kev

lar 2

9 15

00d

Kev

lar 2

9 30

00d

Kev

lar 2

9 60

00d

Kev

lar L

T 40

0d K

evla

r LT

400d

Kev

lar 4

9 14

20d

Kev

lar 4

9 11

40d

Twar

on 2

200

1270

dt K

evla

r 49

1420

d Tw

aron

220

0 15

80dt

Kev

lar 4

9 38

0d K

evla

r 49

195d

Kev

lar 4

9 38

0d Tw

aron

105

5 40

5dt

Kev

lar 4

9 19

5d K

evla

r 49

195d

Kev

lar 4

9 38

0d

Kev

lar 2

9 15

00d

Kev

lar 2

9 30

00d

Kev

lar 2

9 60

00d

Kev

lar L

T 40

0d K

evla

r LT

400d

Kev

lar 4

9 14

20d

Kev

lar 4

9 11

40d

Twar

on 2

200

1270

dt K

evla

r 49

1420

d Tw

aron

220

0 15

80dt

Kev

lar 4

9 19

5d

Kev

lar 4

9 19

5d K

evla

r 49

380d

Twar

on 1

055

405d

t K

evla

r 49

195d

Kev

lar 4

9 19

5d K

evla

r 49

380d

4.0

9.8

12.4

3.5

3.1

6.2

7.3

7.2

6.5

6.4

5.5

1.7

5.1

4.9

2.0

1.8

2.2

136

333

420

122

105

210

248

244

220

215

187

58 173

166

68 61 75

12.8

28.0

33.5

7.0

6.0

12.0

13.4

13.3

12.8

12.0

11.0

3.0

8.7

8.0

4.0

3.9

4.8

0.33

0.71

0.85

0.18

0.15

0.30

0.34

0.34

0.33

0.30

0.28

0.08

0.22

0.20

0.10

0.10

0.12

70 900

890

650

650

900

750

750

900

900

1000

200

650

650

230

200

300

900

1420

600

600

600

900

800

800

900

900

100

200

650

650

230

200

300

X X X X X X X

335

328

328

143

124

181

181

81 120

220

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

5351

352

5352

353

5353

354

5354

357

372

383

5383

384

5384

386

5386

388

5388

Plai

nPl

ain

Plai

n4H

Sat

in4H

Sat

inPl

ain

Plai

nPl

ain

4x4

Twill

5H S

atin

5H S

atin

Bask

et 4

x4Ba

sket

4x4

Bask

et 4

x4Ba

sket

4x4

Bask

et 8

x8Ba

sket

8x8

22 17 17 17 17 13 13 11 73 16 16 28 28 27 27 40 40

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

Twar

on 1

055

405d

t K

evla

r 49

1140

d Tw

aron

220

0 12

70dt

Kev

lar 4

9 11

40d

Twar

on 2

200

1270

dt K

evla

r 49

1420

d Tw

aron

220

0 15

80dt

Kev

lar 4

9 14

20d

Kev

lar 4

9 19

5d K

evla

r 49

2160

d Tw

aron

220

0 22

00dt

Kev

lar 4

9 14

20d

Twar

on 2

200

1580

dt K

evla

r 49

2160

d Tw

aron

220

0 22

00dt

Kev

lar 4

9 14

20d

Twar

on 2

200

1580

dt

Twar

on 1

055

405d

t K

evla

r 49

1140

d Tw

aron

220

0 12

70dt

Kev

lar 4

9 11

40d

Twar

on 2

200

1270

dt K

evla

r 49

1420

d Tw

aron

220

0 15

80dt

Kev

lar 4

9 14

20d

Kev

lar 4

9 19

5d K

evla

r 49

2160

d Tw

aron

220

0 24

20dt

Kev

lar 4

9 14

20d

Twar

on 2

200

1580

dt K

evla

r 49

2160

d Tw

aron

220

0 24

20dt

Kev

lar 4

9 14

20d

Twar

on 2

200

1580

dt

2.2

5.2

5.2

5.2

5.2

4.9

4.9

5.2

3.8

9.1

9.1

10.7

10.7

13.9

13.9

15.5

15.5

75 176

176

176

176

166

166

176

129

309

309

363

363

471

471

526

526

4.6

9.8

10.7

9.3

9.7

9.8

10.0

10.0

7.0

13.0

13.0

19.0

19.0

26.4

26.4

27.6

26.9

0.12

0.25

0.27

0.24

0.25

0.25

0.25

0.25

0.18

0.33

0.33

0.48

0.48

0.67

0.67

0.70

0.68

300

750

800

660

750

650

550

410

520

920

920

1360

1360

1800

1820

1900

1830

300

700

800

650

750

650

550

700

550

970

970

1300

1360

1500

1500

1700

1790

X X X X X

220

281

281

285

285

500

500

540

900

900

1050

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.

56

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

431

702

704

5704

705

706

707

710

712

5712

713

5713

720

722

724

5724

726*

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

n

31 21.6 31 31 31 34 31 24 12 12 31 31 20 22 24 24 26

31 21.6 31 31 31 34 31 24 12 12 31 31 20 22 24 24 26

Kev

lar L

T 40

0d

Kev

lar 1

29 1

000d

K

evla

r 129

840

d Tw

aron

204

0 93

0dt

Kev

lar K

M2

850d

Kev

lar K

M2

600d

Kev

lar K

M2

600d

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

evla

r 129

142

0d K

evla

r 129

142

0d K

evla

r 129

100

0d Tw

aron

204

0 11

00dt

Kev

lar 1

29 8

40d

Kev

lar L

T 40

0d

Kev

lar 1

29 1

000d

Kev

lar 1

29 8

40d

Twar

on 2

040

930d

t K

evla

r KM

2 85

0d K

evla

r KM

2 60

0d K

evla

r KM

2 60

0d K

evla

r 29

1500

d K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

Kev

lar 2

9 10

00d

Twar

on 2

040

1100

dt K

evla

r 129

142

0d K

evla

r 129

142

0d K

evla

r 129

100

0d Tw

aron

204

0 11

00dt

K

evla

r 129

840

d

3.1

5.6

6.8

6.8

6.9

5.4

4.8

9.7

9.1

9.1

8.2

8.2

7.6

8.5

6.2

6.2

5.8

105

190

231

231

234

183

163

324

309

309

278

278

259

289

210

210

200

6.0

10.1

13.9

13.8

12.0

9.8

8.6

19.4

16.5

16.5

16.8

16.3

13.8

15.8

11.4

11.0

10.2

0.15

0.25

0.35

0.35

0.31

0.25

0.22

0.49

0.42

0.42

0.43

0.41

0.35

0.40

0.29

0.28

0.26

570

650

850

900

900

750

700

1100

1200

1200

780

900

1000

600

760

760

850

570

700

1100

950

950

900

800

1200

1200

1200

1000

900

1000

900

780

780

950

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

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

* S

tyle

is b

eing

pha

sed

out,

see

ww

w.jp

scom

posi

tem

ater

ials

.com

for p

oten

tial r

epla

cem

ents

.

57

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

5726

727

728

5728

729

730

731

5731

732

735

736

737*

739

740

741

741M

L57

41

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nBa

sket

2x2

Bask

et 2

x2Pl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

n

26 26 17 17 17 22 31 31 32 35 36 28 39 40 11 22 11

26 26 17 17 17 22 31 31 32 35 36 28 36 40 11 22 11

Twar

on 2

040

930d

t K

evla

r 129

100

0d K

evla

r 29

1500

d Tw

aron

204

0 16

80dt

Kev

lar 1

29 1

420d

Kev

lar 2

9 10

00d

Kev

lar 1

29 1

000d

Twar

on 2

040

1100

dt K

evla

r 29

400d

Kev

lar 2

9 15

00d

Kev

lar 1

29 1

420d

Kev

lar K

M2

600d

Kev

lar 2

9 15

00d

Kev

lar 2

9 20

0d K

evla

r 29

3000

d K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

Twar

on 2

040

930d

t K

evla

r 129

100

0d K

evla

r 29

1500

d Tw

aron

204

0 16

80dt

K

evla

r 192

142

0d K

evla

r 29

1000

d K

evla

r 129

100

0d Tw

aron

204

0 11

00dt

Kev

lar 2

9 40

0d K

evla

r 29

1500

d K

evla

r 129

142

0d K

evla

r KM

2 60

0d K

evla

r 29

1500

d K

evla

r 29

200d

Kev

lar 2

9 30

00d

Kev

lar 2

9 30

00d

Twar

on 1

000

3360

dt

5.8

6.7

6.6

6.9

6.6

5.6

7.9

8.1

3.2

14.1

14.1

4.4

15.2

2.1

8.5

18.8

8.5

197

227

224

234

224

190

268

275

108

478

478

150

517

71 288

639

288

10.1

12.3

12.7

12.1

12.8

11.6

15.2

16.1

6.2

25.4

26.3

8.3

25.3

5.2

16.1

29.0

15.0

0.26

0.31

0.32

0.31

0.33

0.29

0.39

0.41

0.16

0.65

0.67

0.21

0.64

0.13

0.41

0.74

0.38

760 910

900

780

900

800

900

900

450

1700

1950

550

2000

340

1100

1700

1100

770

980

900

800

900

800

900

900

450

1800

2000

575

1800

330

1150

1800

1150

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

ion,

ple

ase

cont

act a

Tech

nica

l Ser

vice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

* S

tyle

is b

eing

pha

sed

out,

see

ww

w.jp

scom

posi

tem

ater

ials

.com

for p

oten

tial r

epla

cem

ents

.

58

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

5741

ML

743

745

5745

745

LCS

5745

LC

S74

774

875

1*75

3*75

457

5475

557

5575

675

976

0

Plai

nTw

ill 4x

4Pl

ain

Plai

nPl

ain

Plai

nPl

ain

Bask

et 8

x8Pl

ain

Bask

et 2

x2Ba

sket

2x2

Bask

et 2

x2Ba

sket

4x4

Bask

et 4

x4Pl

ain

Bask

et 4

x4Ba

sket

2x2

22 40 17 17 17 17 10 48 29 34 21 21 21 21 28 24 30

22 40 17 17 17 17 10 48 29 34 21 21 21 21 28 24 30

Twar

on 1

000

3360

dt K

evla

r 29

3000

d K

evla

r 29

3000

d Tw

aron

100

0 30

00dt

K

evla

r 29

3000

d Tw

aron

100

0 30

00dt

K

evla

r 29

3000

d K

evla

r 29

1500

d K

evla

r KM

2 60

0d K

evla

r KM

2 60

0d K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

K

evla

r 29

3000

d Tw

aron

100

0 33

60dt

K

evla

r KM

2 40

0d K

evla

r 29

3000

d K

evla

r 29

1420

d

Twar

on 1

000

3360

dt K

evla

r 29

3000

d K

evla

r 29

3000

d Tw

aron

100

0 30

00dt

K

evla

r 29

3000

d Tw

aron

100

0 30

00dt

Kev

lar 2

9 30

00d

Kev

lar 2

9 15

00d

Kev

lar K

M2

600d

Kev

lar K

M2

600d

Kev

lar 2

9 30

00d

Twar

on 1

000

3360

dt

Kev

lar 2

9 30

00d

Twar

on 1

000

3360

dt K

evla

r KM

2 40

0d K

evla

r 29

3000

d K

evla

r 29

1420

d

18.8

16.5

13.3

13.4

15.5

15.5

6.5

18.8

4.4

5.3

16.5

16.2

16.3

16.2

2.9

18.0

11.8

639

559

451

454

524

524

220

637

149

180

559

549

554

549

98 610

400

29.0

29.0

25.3

24.2

25.0

25.0

12.0

32.1

7.9

8.9

29.0

30.0

27.9

30.0

5.6

30.0

21.1

0.74

0.74

0.64

0.61

0.64

0.64

0.30

0.82

0.20

0.23

0.74

0.76

0.71

0.76

0.14

0.76

0.54

1700

3200

1200

1700

1600

1600

900

2200

650

750

2000

2000

2000

2000

800

2300

850

1800

3200

700

1800

1800

1800

1000

2300

700

850

2000

2000

2000

2000

600

2000

600

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.

* S

tyle

is b

eing

pha

sed

out,

see

ww

w.jp

scom

posi

tem

ater

ials

.com

for p

oten

tial r

epla

cem

ents

.

59

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

766

767

768

5768

775

779

780*

782*

785

787

791

4000

*40

15*

401

5ML*

4023

*40

29*

5719

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

Twill

2x2

Plai

nPl

ain

Plai

nPl

ain

Plai

nPl

ain

34 28 28 28 31 70 20 22 20 23 26 18 22 44 23 29 19.5

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Kev

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5.4

4.4

3.6

3.6

6.8

3.7

4.4

4.3

4.4

5.1

5.7

3.7

4.6

9.0

3.5

4.5

4.3

184

150

122

122

231

122

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146

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173

194

125

156

306

119

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9.8

7.8

6.5

6.5

11.8

7.6

7.6

7.5

7.6

8.7

9.6

7.3

8.5

16.6

6.9

8.4

7.5

0.25

0.20

0.17

0.17

0.30

0.19

0.19

0.19

0.19

0.22

0.24

0.19

0.22

0.42

0.18

0.21

0.19

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350

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800

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1100

600

700

600

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X X X X X X X X X X X X X

Aram

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s

The

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rics.

Act

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For a

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info

rmat

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cont

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Tech

nica

l Ser

vice

Rep

rese

ntat

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(864

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-350

6.

* S

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X

Aram

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Act

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Tech

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Rep

rese

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(864

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6.

* S

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.

Sty

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Wei

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Aram

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Wei

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al

Serv

ice

Rep

rese

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ive,

(864

) 224

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6.

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768

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0.9

1.7

1.8

2.0

2.1

2.2

2.2

2.9

3.1

3.2

3.4

3.5

3.6

3.6

3.6

3.6

3.7

31 58 61 68 71 75 75 99 105

109

116

119

122

122

122

122

126

779

4000

290

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737

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354

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3.7

3.7

4.0

4.3

4.3

4.4

4.4

4.4

4.4

4.4

4.5

4.6

4.7

4.8

4.9

4.9

4.9

126

126

136

146

146

150

150

150

150

150

153

156

160

163

167

167

167

173

173

177

177

177

177

177

180

184

184

187

190

190

194

197

197

200

323

724

5328

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747

5724

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729

727

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5704

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5728

5931

5324

324

6.2

6.2

6.4

6.5

6.5

6.5

6.6

6.6

6.7

6.8

6.8

6.8

6.9

6.9

7.0

7.2

7.3

211

211

218

221

221

221

224

224

228

231

231

231

235

235

238

244

248

348

787

352

353

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766

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5726

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5.1

5.1

5.2

5.2

5.2

5.2

5.2

5.3

5.4

5.4

5.5

5.6

5.6

5.7

5.8

5.8

5.9

720

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296

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7.6

7.9

8.1

8.2

8.2

8.5

8.5

8.5

9.0

9.1

9.1

9.1

9.1

9.4

9.7

9.8

10.7

259

269

275

279

279

289

289

289

306

309

309

309

309

320

330

333

364

62

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Aram

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The

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Act

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For a

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ple

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cont

act a

Tec

hnic

al

Serv

ice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

5384

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10.7

11.8

12.4

13.3

13.4

13.6

13.9

14.1

14.1

15.2

15.3

15.5

15.5

15.5

16.2

16.3

16.5

364

401

422

452

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473

479

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517

520

527

527

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18.8

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561

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639

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4.0

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5.2

5.6

6.0

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6.5

6.5

6.9

7.0

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0.05

0.08

0.10

0.10

0.12

0.12

0.13

0.14

0.15

0.15

0.16

0.17

0.17

0.18

0.18

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7.5

7.5

7.6

7.6

7.6

7.8

7.9

8.0

8.3

8.4

8.5

8.6

8.7

8.7

8.9

9.3

0.19

0.19

0.19

0.19

0.19

0.19

0.20

0.20

0.20

0.21

0.21

0.22

0.22

0.22

0.22

0.23

0.24

0.24

0.24

0.25

0.25

0.25

0.25

0.25

0.25

0.25

0.26

0.26

0.26

0.26

0.27

0.28

0.28

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730

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11.6

11.8

12.0

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12.1

12.3

12.7

12.8

12.8

12.8

12.9

13.0

13.0

13.3

0.29

0.30

0.31

0.31

0.31

0.31

0.31

0.31

0.31

0.32

0.33

0.33

0.33

0.33

0.33

0.33

0.34

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9.4

9.6

9.7

9.8

9.8

9.8

9.8

10.0

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10.1

10.2

10.2

10.2

10.7

11.0

11.0

11.4

354

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13.4

13.8

13.9

14.8

15.0

15.2

15.8

16.1

16.1

16.3

16.5

16.5

16.6

16.8

19.0

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0.34

0.35

0.35

0.38

0.38

0.39

0.40

0.41

0.41

0.41

0.42

0.42

0.42

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0.48

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Aram

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dex

The

phys

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Act

ual v

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For a

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onal

info

rmat

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ple

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cont

act a

Tec

hnic

al

Serv

ice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

64

Sty

le

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25.0

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25.3

25.4

26.3

26.4

26.9

27.6

27.9

28.0

29.0

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0.54

0.61

0.64

0.64

0.64

0.65

0.65

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0.67

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0.68

0.70

0.71

0.71

0.74

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0.74

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0.76

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Aram

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dex

The

phys

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Act

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For a

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ple

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cont

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Tec

hnic

al

Serv

ice

Rep

rese

ntat

ive,

(864

) 224

-350

6.

65

S

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Cou

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15.5

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0.39

0.46

0.44

0.61

0.16

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0.24

0.13

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0.36

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900

1100

950

1500

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15.8

10.9

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13.6

11.8

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14.9

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9.4

12.9

14.7

4.0

5.5

2.5

3.4

3.3

3.5

3.4

3.6

3.6

3.1

2.9

3.7

3.3

2.1

5.28

7.42

8.15

8.15

9.21

9.55

9.55

9.55

9.93

11.7

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9.74

9.21

9.69

1.11

1.40

3.04

2.10

2.61

2.08

2.61

2.27

3.25

4.25

4.68

1.81

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Selected Conversions and FormulaeUS to SI SI to US

1 oz/yd = 33.91 g/m 1 g/m = 0.295 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 = 4.45 N

1 psi = 6.89 x 10 MPa 1 ksi = 6.89 MPa 1 MPa = 1 N/mm 1GPa = 1000 MPa

1 denier = 0.111 Tex 1 Tex = 9 denier 1 Tex = 496.24 yd/lb

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 = 4.89 kg/m 1 kg/m = 0.204 lb/ft1 lb/ft = 16.05 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 8.756 = N/cmThickness in x 25.400 = mmMullen Burst lb/in x 0.007 = MPaPorosity cfm x 0.508 = cm/cmArea yd x 0.8361 = m

2 2 2 2

2-3

-1 -1 -1 -1 -1

2 23 3

2 23 3

2 2

2

2 22

69

NOTES

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(864) 260-6581 Fax

70