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JPS Composite MaterialsCorporate Headquarters and US Operations
2200 South Muray 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: Yarn to Fabric................................ 12Specifications & Standards.................................................. 14
FIBERGLASS PRODUCTS................................................. 16Physical Properties of E-glass............................................. 16Physical Properties of S-2 ® Glass......................................17Physical Properties of Insulbatte ®, Tempmat ®..................18Fiberglass Fabric Applications............................................. 19Fiberglass Fabric Finishes................................................... 20Finishes for Electrical Laminates..........................................21Finishes for Aerospace, Conform & Advanced Composites.22Finishes for Boat & Tooling / Surf.........................................24Finishes for EIFS................................................................. 24Finishes for Filtration Fabrics...............................................25Finishes for Insulation & Glastex Fabrics............................ 26Other Finishes & Special Processes....................................27
FIBERGLASS FABRIC CONSTRUCTIONS........................ 28Electrical Fiberglass Fabrics................................................ 28Aerospace, Conform & Advanced Composite Fabrics.........33Fiberglass Reinforced Plastics (FRP) - Boat & Tooling Fabrics.....................................................37Filtration Fabrics...................................................................39Filtration Finished Fabrics....................................................40Insulation Coating Fabrics................................................... 41Insulation GlasTex Fabrics...................................................42EIFS Mesh Fabrics.............................................................. 43Fiberglass Fabric Weight Index........................................... 44Fiberglass Fabric Thickness Index...................................... 47
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ASTROQUARTZ ® PRODUCTS.........................................50Physical Properties of Astroquartz ® II................................ 51Astroquartz ® Applications...................................................51Design Considerations for Astroquartz ® Fabric Selection..52Astroquartz ® II & III Fabric Finishes................................... 52Astroquartz ® II Chopped Fiber........................................... 53ASTROQUARTZ ® II & III FABRICS................................... 54Astroquartz ® Mat Style No. 550......................................... 55Astroquartz ® II Roving....................................................... 55Astroquartz ® II Sewing Thread.......................................... 56Astroquartz ® II Yarn........................................................... 57Testing Properties of:Astroquartz ® II 350ºF Epoxy Laminates.............................58Astroquartz ® II Toughened Epoxy Laminates.................... 58Astroquartz ® II Polyimide Laminates................................. 59Astroquartz ® II Lightweight 8 Harness Satin Fabric........... 59Astroquartz ® II Roving....................................................... 59Astroquartz ® II Unidirectional Fabric.................................. 60Astroquartz ® II Dielectric Properties...................................60Astroquartz ® III Plain Weave Fabric................................... 61Astroquartz ® III 8 Harness Satin Fabric..............................61
ADVANCED MATERIALS PRODUCTS...............................62Physical Properties of Aramid Fibers...................................62Physical Properties of Selected Advanced Performance Fibers............................................. 62Advanced Materials Applications......................................... 63Advanced Materials Fiber Nomenclature............................ 63Finishes for Advanced Materials.......................................... 64
ADVANCED MATERIALS FABRIC CONSTRUCTIONS..... 65Kevlar ® 49 Fabrics............................................................. 65Twaron ® Fabrics................................................................ 66Kevlar ® 29, 129, 159, LT, KM2, KM2+, X300, and Comfort XLT Fabrics........................................... 68Spectra ® Fabrics................................................................72S-2 ® Glass Rovings and Aramid Hybrid Fabrics................ 73
Technical References - English........................................... 74Technical References - Metric............................................. 75Technical References - Common Projectile Caliber Sizes...76Selected Conversions & Formulae...................................... 77
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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 and tooling, advanced composites, ballistics, architecture and construction, and sporting goods. Our materials are readily adaptable to unlimited design opportunities.
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 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, but 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 variable 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 are intended as a general guide and are 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 fiber glass weights, as well as yarn counts available in aramid and polymer fibers, 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 fiber glass and high performance fabrics. The technology, however, is advanced to incorporate specialized precision equipment to meet the exacting demands of modern applications. Almost any weave can be woven, however for industrial there are seven basic patterns including: Plain, Basket, Leno, Four Harness Satin (Crowfoot), Eight Harness Satin, High Modulus, 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 bushing. A strand is produced by combining many individual continuous filaments (from 51 to 1632) depending on bushing size and end-use requirement. The filaments are coated with a lubricant or binder to protect them from damage during processing and weaving.
FormulationsGlass fibers are made from different formulations: “E” (electrical) being the most common all-purpose glass, while “S” (high-strength) is made for special applications. Astroquartz ® II and III quartz fiber products are the purest form of silica. The chemical composition of these glass formulations is shown on the next page.
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COMPOSITION OF TYPICAL GLASSES (%) by weight
“E” “S” 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, the other numerical.
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 2/2
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 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).
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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 150-2/2 Where: E = Electrical Glass
C = Continuous Filament
G = Average Filament Diameter (see table, page 6)
150 = 15,000 Yd/Lb (Nominal) of Basic Strand
2/2 = Four Strands in the Twisted and Plied Yarn (2x2)
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 2 x 2The results of this computation must always be considered approximate because yards per pound are reduced slightly in the twisting and plying operations.
= 3750 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.
ConstructionThis is determined by the number of warp yarns (machine direction) and fill yarns (cross-machine direction) per inch of the fabric.
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 performance characteristics.
FinishMost industrial applications require that fabric be used with another material. For compatibility with other materials, a finish or after treatment is often applied to the fabric. See the finish sections for descriptions of various treatments.
YARN CONSTRUCTION
Twisting/PlyingThis process serves to control the yarn strength, diameter, weight, and flexibility. The 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 can may cause processing difficulties. Many glass fabrics are woven from single yarns as received from the yarn producers. The filament diameter and the number of filaments in the base strand will also affect the yarn strength, diameter and flexibility.
WarpingThe warping operation in producing woven fabric is accomplished by laying the fibers in parallel order. A specified number of threads per inch are drawn from a creel and wound on a warp beam. Several warp beams are then combined to provide the designated number of threads per inch required in the fabric specification. This entire system of parallel threads is wound on one loom beam to become the “warp” or lengthwise system of threads in the fabric.
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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.
EnteringThe entering operation arranges yarn for weaving in the warp direction. In this process, the warp yarns are threaded from the loom beam through the needle eyes on the proper harnesses to achieve the desired pattern or design in the fabric. The warp yarn is then drawn through a reed that is the final coating of the warp thread count. The reed is also to place the filling yarns in their proper position.
WeavingWeaving consists of interlacing a series of fiberglass 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.
WeavesThe 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 as
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civilization. All standard fabric weaves can be produced withfiberglass, aramid, Astroquartz ®, polymer and carbon yarns.
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. 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 each other. The basket weave is more pliable, flatter, and stronger than the plain weave, but is not as stable.
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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 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 andunder one.
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. It is generally produced in the6 oz/sqyd to 18 oz/sqyd weight range.
High Modulus Weave
The high modulus weave is used where high impact resistance and high strength are required. The weave eliminates the interlacing of structural yarns, thereby reducing crimp and shear factors. This special weave is the most pliable and conforms most readily to highly contoured planes.
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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.
The Manufacturing Process:Yarn to Fabric
1. WarpingInput yarn is transferred from the bobbin creel to section beams. The section beams constitute the machine direction or thread sheet segment of yarn in the loom. Several section beams are produced and consolidated into a “set”, which provides the input for slashing.
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2. SlashingSlashing combines the warp ends of the set’s multiple section beams in a single warp or loom beam for weaving. Sizing is applied to the individual warp ends to minimize filament damage during handling and weaving.
3. EnteringIn the entering state the warp beam is setup for installation on the loom. A warp can containover 4,500 individual ends, depending on the design of thestyle. Each warp end is drawn through a drop wire, heddles and areed by hand or by machine. The drop wire, heddles and reed work tomechanically arrange and control thewarp yarn during weaving on the loom.
4. WeavingThe warp beam is installed on the loom, then either rapier technology for heavy fabrics or air jet technology for lighter weight fabrics is used to interlace the filling yarns at 90º angles to the warp ends. Once woven the fabric, called “greige fabric”, is then wound onto a roll ready for heat cleaning for glass or scouring for organic fabrics.
5. Heat CleaningGlass fabrics are processed through a caramelizer or coronizer to oxidize the organic binders and sizings from prior steps. The fabric then wound onto a porous steel drum, called a mandrel, and placed in a large batch oven and exposed to high heat. The heat flows around the exterior of the fabric, as well as through the mandrels to ensure complete exposure. The heat removes
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all organics, leaving pure clean glass fabric. Organic, polymer based, fabrics are not heat cleaned.
6. 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.
Specifications and StandardsJPSCM fabrics are designed to meet the requirements of a wide range of end users, including commercial and governmental specifications for composite reinforcement fabrics. This standards and specifications. Listed below are a partial offering of the standards and specifications we manufacture towards. For adherence to a specific standard or specification not listed, please inquire not listed please contact customer service or technical support.
AMS-3824 - Covers basic forms of finished fiberglass fabrics used alone or components in other materials.
AMS-3846 - Covers quartz fabrics in woven form finished for resin laminates.
AMS-3902 - Covers cloth woven from high modulus, continuous multifilament aramid yarn.
AMSC-9084 - Covers the requirements for woven, cleaned, and finished glass fabrics for use in resin laminates and sandwich materials.
ASTM-D-579 - Standard specifications for greige woven glass fabrics and their testing.
ASTM-D-1668 - Covers open mesh woven glass fabrics used for membrane waterproofing and built up roofing.
ASTM-D-3659 - Covers flame spread in self extinguishing EIFS finishes.
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ASTM-D-4029 - Standard specifications for woven E-glass fabrics for reinforcement use.
ASTM-E-2098 - Covers Alkali resistance of finished fabrics used in Exterior Insulation Facing Systems (EIFS) for building products.
BMS 9-3 - Covers Boeing Commercial Airplane Company’s requirements for woven, cleaned, and finished E-glass fiber fabrics for use in aircraft structures and repair.
IPC-4412 - Covers woven and finished glass fabrics for use in printed circuit boards.
MIL-C-20079 - Covers glass and tape used as lagging material over thermal insulation and for hull insulation board.
MIL-C-22787 - Covers vinyl coated base glass fabrics.
MIL-DTL-44050 - Covers cloth woven with high modulus, continuous, multifilament yarn.
MIL-DTL-46593 - Projectile specifcitations for armor testing.
MIL-DTL-62474 - Covers aramid fabric reinforced plastic laminate for use in composite armor systems.
MIL-I-24244 - Covers thermal insulation with special corrosion and chloride requirements.
MIL-PRF-64154 - Covers phenolic laminates made with glass fabric for use in composite armor systems.
MIL-R-7575 - Polyester resin low pressure laminates made with glass fabric reinforcement.
MIL-R-9300 - Covers epoxy resin low pressure laminates made with glass fabric reinforcement.
MIL-S-662 - V-50 ballistic test for armor.
MIL-Y-1140 - Covers basic forms of untreated glass yarns and fabrics used alone or as components of other materials.
NRC 1.36 - Covers the requirements of the Nuclear Regulatory Certification of GlasTex fabrics.
USCG Subpart 164-009 - Covers non-combustible material for use in merchant vessels.
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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-2 ®* Glass* S-2 ® is a registered trademark of AGY Corporation
Approximate 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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Physical Properties of Insulbatte ®, Tempmat ®Insulbatte ® and Tempmat ® are registered trademarks of JPS Industries
Insulbatte ® and Tempmat ® are mechanically bonded, noncorrosive, noncombustible, nonalkaline, chemically stable fabrics mat blankets. The 100% E-glass mats are manufactured in web form through a needling process to form thicknesses of 1/4”, 1/2”, and 1”. E-glass fibers are accurately chopped to provide maximum density, high insulation, and strong physical properties at temperatures up to 1200ºF.
Insulbatte ® and Tempmat ® are commonly used in complex applications in oil refineries, steam and gas turbine operations, exhaust systems and commercial marine applications as well as applications for the U.S. Navy andU.S. Coast Guard. In addition, the mats are used as insulators in automotive applications and to replace rigid block nuclear power plants.
Insulbatte ® and Tempmat ® meet the requirements of MIL-I-16411 Type II, NRC 1.36, MIL-I-24244, USCG 164-009, and all pertinent automotive specifications.
Insulbatte ® / Tempmat® Bonded Glass Fiber Mat Style 1006 1050 1031 1032 1033 1034Thickness (in) 1/4 1/2 1 1 1 3/4
Weight (oz/sqft) 4 6 15 15 17 14
Width (in) 60 60 60 60 60 60
Roll Length (ft) 150 75 45 45 45 45
Area (sqft/roll) 750 375 225 225 225 225
Approx. Roll 180 140 221 221 221 221 Weight (lb)
Note: Width and roll length can be made-to-order. All valuesabove are nominal values. S/1036 1” is double needled.
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Physical PropertiesService Temperature........................................... Up to 1200ºFFire Resistance...................................................IncombustibleDensity (Approximate)....................................................9 lb/cftLoss in Weight at 1200ºF........................................... Up to 2%Moisture Absorption..................................................Negligible
Thermal Conductivity“K” Value at 9.1 lb/cft At 300ºF..........................................................................0.40 K At 500ºF..........................................................................0.50 KAt 700ºF..........................................................................0.65 KK = (btu/sqft/hr/ºF/in)R-values available upon request
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 provide high strength, dimensional stability, fire resistance, and low cost making them ideal for use as reinforcements in foils, plastic films, and other protective coatings. Fiberglass 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.
ConstructionFiberglass fabrics can found in everything from industrial strength tapes to wall-board and bridge construction. Fiberglass scrims are used to reinforce paper and films used for insulation facings, to provide dimesional stability to asphalt roofing and roadway materials. In architecturalapplications fiberglass fabrics provide strength and sustainability to the exterior facades of commercial buildings, and reinforcement for commercial roofing systems. Fiberglass reinforced material are often used to cover outrecreational facilities, among other structures.
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ElectricalFiberglass fabrics offer outstanding performance to the electrical industry. Fiberglass fabrics are used in electrical laminates, antennas and printed circuit boards because they offer high strength, dimensional stability, temperature resistance and excellent electrical properties for low cost. Fiberglass fabrics may be coated with epoxies, silicones, rubber, PTFE, polyimides, neoprene and many other polymers. Fiberglass fabrics can be found in printed circuit boards, antennas, high voltage generators, transformers, switches, cables and many other electrical applications.
Structural ApplicationsDue to their high strength, dimensional stability and low cost, fiberglass fabrics are often used in the aerospace, automotive industries for structural applications. Fiberglass fabrics areused as reinforcements in highly engineered composite materials in many of the worlds leading aircraft, automobiles, buildings, bridges, roadways and sporting goods, among countless other applications.
Thermal InsulationStrength retention at high temperatures, corrosion and fire resistance and ease of handling make fiberglass fabrics an important material for thermal insulation. The U.S. Navy and commercial shipyards use fiberglass almost exclusively for pipe lagging and for thermal pad cover applications.
Fiberglass Fabric FinishesFiberglass fabrics are available with a variety of finishes and treatments.
Greige Loom state fabric that includes organic binders and size applied to the yarn prior to weaving.
Carmelized Partially heat cleaned fabric in which the organic binders and size are only partially volatilized.
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Finished Fully heat cleaned fabric treated with a coupling agent that provide the a chemical bond between the fiberglass surface and various matrix resins.
APS Technology Treatment process that spreads and flattens both the warp and fill yarns. Provides uniform fiber distribution, thinner fabrics with flatter knuckles, smoother surface and improved mechanical properties.
Weave Set Also called tie coats, finishes added to greige fabrics to improve weave stability and adhesion of various coatings to the fabric.
The following pages offer recommended finishes based on end use market application, including Electrical Laminates, Aerospace and Advanced Composites, Boat and Tooling, Surf, EIFS and Construction, Filtration, Insulation and Glastex, as well as other special finishes and processes for customer directed end use applications.
Finishes for Electrical LaminatesA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.
Finish Matrix PerformanceCode Resin Features
CS-309 Polyimide Designed for polyimide resins.
CS-616 Melamine Silane finish applied to partially heat cleaned fabrics. Fabric has a light tan cast.
CS-718 Epoxy Proprietary silane finish that provides good moisture resistance.
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Finishes for Electrical Laminates (cont.)
A partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.
Finish Matrix PerformanceCode Resin Features
CS-745 Polyimde, Epoxy Multifunctional finish designed. BT, Cynate Ester for lead free and CAF resistant applications.
Z-6040 Epoxy Offers good resistance to blistering and measling in solder dip or etching solutions.
9827 Epoxy, Polyimide Blended silane finish for a Bismaleimide broad spectrum of high performance resin systems.
9837 Vinyl, Polyester Silane finish with vinyl Vinyl Ester, Epoxy functionality for resins cured Bismalemide via vinyl addition.
Finishes for Aerospace, Conform & Advanced CompositesA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.
Finish Matrix PerformanceCode Resin Features
CS-310 Epoxy Recommended for advanced composite and aerospace applications
CS-550 Polyester, Epoxy, Volan/Silane finish for Phenolic structural applications.
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Finishes for EIFSFlexmesh™ PerformanceName FeaturesStandardflex™ High impact strength for high maintenance areas.
Duraflex™ Good “hand” for flat wall work.
Ultraflex™ Excellent for detail and high end work.
Finishes for Aerospace, Conform & Advanced Composites (cont.)Finish Matrix PerformanceCode Resin FeaturesS-550 Epoxy, Phenolic, Good conformabilty and hand. Melamine Fabric has a light green cast
CS-616 Melamine Silane finish applied to partially heat cleaned fabrics. Fabric has a light tan cast.
CS-724 Epoxy Specifically developed finish for structural composites.
CS-767 Polyimide, BT Multifunctional capacity for use Epoxy with all major resin systems.
933 HTS Polyimide, Epoxy Excellent high temperature Phenolic, BT and moisture resistance.
S-977 Epoxy, Polyester Specifically developed finish Phenolic, Melamine for structural composites.
1059 HT Polyimides Designed for high temperature (700ºF) polyimide systems.
1069 HT Polyimide, BT, Recommended for low Dk, Cynate Ester, high Tg resin systems.
A-1100 Phenolic, Epoxy Reactive amino silane.
Z-6040 Epoxy Good wet strength retention and electrical properties.
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Finishes for Boat & Tooling / SurfA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.
Finish Matrix PerformanceCode Resin Features
S-910 Polyester Laminates have good clarity & high wet strength retention.
S-912 Polyester Recomended for marine and Epoxy surf applications.
F3 Polyester Traditional Volan-A type-finish.
F16 Epoxy Recomended for advanced Polyester composite, marine and aerospace applications.
Great Polyester High mechanical White properties, long term wet strength retention, clarity, drapability, and fast wet out.
Volan Polyester, Epoxy Methacrylate Chromium complex finish. Laminates have a green cast.
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.
24
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 PerformanceCode Features
1200 Excellent acid resistance and high Acid-Flex™ flexibility at elevated temperature. The finish is hydrophobic, oleo phobic, and is dust and dirt repellent.
1300 Designed for lamination to PTFE filmsAcid-Bond™ Excellent acid resistance and high flexibility at elevated temperature.
1400 Excellent chemical and heat resistance.Ultra-Flex™ Ideal for finishing filtration bags in baghouse applications.
1625 Excellent acid resistance and high flexibility at elevated temperture. Laminatable with PTFE membranes.
9892 Tritemp finish - special formula blend of silicone, fluorocarbon & graphite for maximum high temperature lubricity of glass fabrics.
9963 Teflon B finish - A fluorocarbon finish with excellent chemical resistance and high temperature lubricity. The finish has a soft hand and meets the challenges of many dust collection and air pollution control problems.
PTFE A fluorocarbon finish with excellent chemical resistance and high temperature lubricity. The finish has a soft hand and meets the challenges of many dust collection and air pollution control problems.
25
Finishes for Insulation & GlasTex FabricsA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.
Finish PerformanceName Features
9383 Treatment to enhance hand and weave setting characteristics.
9480 Aluminum foil is laminated to GlasTex fabrics with a fire-retardant thermoplastic adhesive. This vapor barrier laminate is specified for shipboard usage as flange fuel spray shields.
9752 Weave set finish for fabric stability and reduction of fiber irritation.
9845 A low smoke treatment over 9383 finish that provides good weave stability.
9957 Dyed red to Federal Color #31158 to indicate a nonasbestos bearing product.
9987 A treatment over 9383 finish that provides oil and water repellency.
9995 GlasTex fabrics are impregnated with a water-activated adhesive for application as a rewettable lagging material. After drying, normal sizing and painting is recommended for permanency.
26
Other Finishes & Special ProceduresA partial list of the available finishes is presented, for additional finishes or to develop an application specific finish, please contact JPSCM.
Finish PerformanceName Features
P-44 Thermomechanical cleaning process. Fabrics possess superior tensile strengths and are white in color.
111 Similar to 210 heat cleaning but is distinguished by lower levels of remaining organic binder.
112 Fully heat cleaned fabric.
210 Carmelized fabric in which organic binders are partially volatilized.
9583 Scour Continuous chemical treatment for size reduction.
Greige Loom state fabric, no additional fabric finish processing.
NPH Neutral pH finish for silicone laminates.
27
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
101
104
106
108
112
113
116
117
119
1035
1037
1044
1047
1065
1067
1067
APS
1070
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
75 60 56 60 40 60 60 54 54 66 70 44 47 56 70 70 60
75 52 56 47 39 64 58 39 50 68 73 44 47 56 70 70 35
ECD
180
0 1/
0EC
D 9
00 1
/0EC
D 9
00 1
/0EC
D 9
00 1
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D 4
50 1
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D 4
50 1
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D 4
50 1
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D 4
50 1
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D 4
50 1
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D 9
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C 1
200
1/0
ECD
E 10
0 1/
0EC
DE
100
1/0
ECD
450
1/0
ECD
900
1/0
ECD
900
1/0
ECD
450
1/0
ECD
180
0 1/
0EC
D 1
800
1/0
ECD
900
1/0
ECD
900
1/2
ECD
450
1/2
ECD
900
1/2
ECD
450
1/2
ECD
450
1/2
ECD
450
1/2
ECD
900
1/0
EC
C 1
200
1/0
ECD
E 10
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DE
100
1/0
ECD
900
1/0
ECD
900
1/0
ECD
900
1/0
ECD
900
1/0
0.48
0.55
0.72
1.40
2.08
2.39
3.09
2.40
2.71
0.88
0.68
5.10
5.44
1.08
0.91
0.88
1.01
16 19 24 48 71 81 105
81 92 30 23 171
184
37 31 30 34
1.0
1.1
1.3
2.4
3.6
3.4
4.0
2.6
3.6
1.1
1.1
5.6
5.8
2.1
1.4
1.3
1.8
0.02
0.03
0.03
0.06
0.09
0.09
0.10
0.07
0.09
0.03
0.03
0.14
0.15
0.05
0.04
0.03
0.05
40 40 45 70 100
120
125
100
45 110
70
40 15 40 40 90 70 120
90 40 130
20
Elec
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ergl
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Fabr
ics
The
phys
ical
pro
perti
es li
sted
are
for g
reig
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ntre
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rics.
Act
ual v
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For a
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ple
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cont
act a
Tech
nica
l Ser
vice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
28
29
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
1078
1080
1081
1125
1131
1141
1142
1161
1165
1167
1180
128
0/10
86
1280
APS
1316
1500
1501
1502
Plai
nPl
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Plai
nPl
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Plai
nPl
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Plai
nPl
ain
Plai
nPl
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Plai
nPl
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Plai
nPl
ain
Plai
nPl
ain
Plai
n
54 60 70 40 120
32 31 100
60 60 60 60 60 61 50 49 52
54 47 60 39 52 21 21 42 52 55 50 60 60 61 20 42 50
ECD
450
1/0
ECD
450
1/0
ECD
450
1/0
ECD
450
1/2
ECD
450
1/0
ECD
E 75
1/0
ECG
37
1/0
ECD
450
1/0
ECD
450
1/2
ECD
450
1/2
ECD
450
1/0
ECD
450
1/0
ECD
450
1/0
ECD
225
1/0
ECD
450
1/0
ECE
110
1/0
ECE
125
1/0
ECD
450
1/0
ECD
450
1/0
ECD
450
1/0
ECG
150
1/0
ECG
150
1/0
ECD
E 75
1/0
ECG
37
1/0
ECD
E 10
0 1/
0EC
G 1
50 1
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G 1
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D 4
50 1
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D 4
50 1
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D 4
50 1
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D 2
25 1
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D 4
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E 11
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E 15
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0
1.41
1.38
1.72
2.65
3.65
4.20
8.37
3.87
3.57
3.82
1.44
1.55
1.54
3.18
0.92
4.84
4.78
48 47 59 90 124
142
285
131
123
129
49 53 53 108
31 164
148
1.7
2.1
2.4
3.6
5.0
7.0
11.1
4.8
4.0
4.4
2.3
2.2
2.1
4.0
2.2
5.9
5.9
0.04
0.05
0.06
0.09
0.13
0.18
0.28
0.12
0.10
0.11
0.06
0.06
0.05
0.10
0.06
0.15
0.15
120
80 120
140
250
400
125
125
170
120
100
100
260
90 20 80 150
125
290
180
160
250
100
100
40 250
Elec
trica
l Fib
ergl
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Fabr
ics
(con
t)
The
phys
ical
pro
perti
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sted
are
for g
reig
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ntre
ated
) fab
rics.
Act
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s m
ay v
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For a
dditi
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info
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ple
ase
cont
act a
Tech
nica
l Ser
vice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
30
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
1503
1504
1634
1647
16
4916
5116
5216
5716
74
1676
1677
1678
2112
2113
2114
2116
2117
Pla
in
Plai
nPl
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Plai
nPl
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Plai
nPl
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Plai
nPl
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Plai
nPl
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Plai
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Plai
nPl
ain
Plai
nPl
ain
64 60 51 51 51 51 52 51 40 56 44 40 40 60 56 60 66
46 50 30 30 38 27 52 32 32 48 38 40 39 56 48 58 55
ECD
E 15
0 1/
0EC
DE
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECD
E 15
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DE
150
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ECG
150
1/0
ECG
150
1/0
ECE
225
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ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
225
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150
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E 15
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G 1
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G 6
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DE
150
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E 22
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D 4
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E 22
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E 22
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0
4.36
4.36
3.11
3.55
4.01
4.31
4.09
2.82
2.84
4.06
3.15
3.20
2.04
2.30
2.69
3.06
3.18
148
148
105
121
136
146
138
96 97 138
105
108
69 78 91 104
108
5.3
4.9
3.7
4.1
4.7
5.3
4.5
3.8
4.0
4.6
3.7
4.3
3.2
3.1
3.3
3.7
3.7
0.14
0.13
0.10
0.11
0.12
0.14
0.11
0.10
0.10
0.14
0.09
0.11
0.08
0.08
0.08
0.09
0.09
220
250
200
90 195
190
125
210
190
200
80 75 160
120
Elec
trica
l Fib
ergl
ass
Fabr
ics
(con
t.)
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.
31
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
2119
2125
2157
2165
2166
2313
2316
2319
2875
3070
3080
3116
3132
3313
3323
6060
7196
Plai
nPl
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Plai
nPl
ain
Plai
nPl
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Plai
nPl
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Plai
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Plai
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Plai
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54 40 60 60 60 60 61 60 40 70 51 58 60 60 60 60 44
50 39 35 52 38 64 61 49 28 70 30 58 60 62 46 60 33
ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
225
1/0
ECE
150
1/0
ECD
E 30
0 1/
0EC
DE
300
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ECD
450
1/2
ECD
450
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E 30
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300
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E 60
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0EC
G 6
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0
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225
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ECG
150
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ECG
75
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ECG
150
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ECG
75
1/0
ECD
450
1/0
ECE
225
1/0
ECE
225
1/0
ECE
150
1/0
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E 30
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0EC
DE
300
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225
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225
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E 30
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0EC
E 22
5 1/
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DE
600
1/0
ECG
67
1/0
2.66
2.54
4.36
3.55
4.60
2.40
3.13
2.72
2.70
2.43
1.57
3.10
2.32
2.48 2.4
1.15
6.72
90 88 148
122
155
81 106
92 91 82 53 105
79 82 81 39 230
3.4
3.6
5.1
4.0
5.5
3.3
3.8
3.4
4.5
3.2
2.3
3.5
2.8
3.3
3.4
1.9
7.9
0.09
0.09
0.13
0.10
0.14
0.08
0.10
0.09
0.11
0.08
0.06
0.09
0.07
0.08
0.09
0.05 0.2
140
120
130
75 185
140
175
180
150
160
75
110
120
200
75 300
140
100
160
140
140
75
Elec
trica
l Fib
ergl
ass
Fabr
ics
(con
t)
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
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
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Thi
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Stre
ngth
(lbf
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W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
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(m
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(m
m)
War
p
Fill
22
7255
7618
7624
7626
7627
7628
7629
7630
7635
7637
7640
7642
7650
7652
7660
7667
7629
0
Plai
nPl
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Plai
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Plai
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Plai
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Plai
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Plai
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Plai
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37 43 44 34 44 44 44 31 44 44 44 44 30 32 30 44 44
37 18 24 32 30 31 34 30 29 22 34 20 23 32 30 31 31
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
50
1/0
ECG
75
1/0
ECG
67
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECG
50
1/0
ECG
37
1/0
ECG
50
1/0
ECG
37
1/0
text
ECG
50
1/0
ECG
50
1/0
ECG
75
1/0
ECG
67
1/0
ECG
67
1/0
6.00
4.95
5.44
5.40
5.87
6.00
6.19
4.84
6.85
6.73
7.60
6.72
6.12
7.60
4.73
6.54
6.27
203
168
184
183
199
203
210
164
232
228
258
228
208
258
160
222
213
7.0
6.5
6.4
6.0
6.5
6.8
7.1
6.0
7.9
8.7
9.8
10.0
7.5
8.7
5.9
7.2
7.0
0.18
0.17
0.16
0.15
0.17
0.17
0.18
0.15
0.20
0.22
0.25
0.25
0.19
0.22
0.15
0.19
0.18
300
335
410
225
250
250
230
250
260
250
260
350
300
125
270
200
200
215
230
225
250
120
250
350
Elec
trica
l Fib
ergl
ass
Fabr
ics
(con
t)
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.
32
S
tyle
W
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Cou
nt C
ount
W
arp
F
ill
W
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Thi
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ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
120
138
139
162
220
232
403
520
880
993
1071
1076
1188
1297
1299
1507
1526
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60 65 64 28 60 48 54 18 50 38 60 60 47 50 50 20 35
58 60 60 16 58 30 50 17 71 67 30 25 30 20 20 10 32
ECD
450
1/2
ECE
225
1/2
ECD
225
1/2
ECE
225
2/5
ECE
225
1/0
ECG
37
1/0
ECG
75
1/0
ECG
75
1/3
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E 15
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D 9
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/0EC
D 9
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/0EC
D 4
50 1
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H 2
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D 4
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D 4
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ECD
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ECE
225
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ECD
225
1/2
ECE
225
2/5
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225
1/0
ECG
75
1/2
ECG
75
1/2
ECG
75
1/3
ECD
E 15
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D 9
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6.66
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5.70
0.71
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12.6
30.
820.
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805.
33
107
226
220
407
109
427
285
295
193
24 20 54 428
28 31 332
181
3.5
6.6
6.5
13.8
3.5
14.6
8.9
9.1
6.0
1.2
1.2
2.9
11.8
2.3
2.2
25.0
5.9
0.09
0.17
0.16
50.
350.
090.
370.
230.
230.
150.
030.
030.
070.
300.
060.
060.
640.
15
125
270
250
700
125
550
250
330
300
45 60 140
680
70 100
75 240
120
260
200
420
120
400
200
330
230
20 25 60 100
10 40 115
200
Aero
spac
e, C
onfo
rm, a
nd A
dvan
ced
Com
posi
te 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.
33
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
1527
1530
1543
1557
1576
1581
1582
1583
1584
1597
1608
1609
1610
1611
1617
1620
1628
Plai
nPl
ain
4H S
atin
4H S
atin
12H
Sat
in8H
Sat
in8H
Sat
in8H
Sat
in8H
Sat
inPl
ain
Plai
nPl
ain
Plai
nPl
ain
Plai
nPl
ain
Plai
n
17 20 49 57 120
57 60 54 44 30 30 32 32 32 30 20 40
17 18 30 30 24 54 56 48 35 30 26 10 28 28 14 20 28
ECG
150
3/3
ECG
150
3/3
ECG
75
1/2
ECG
150
1/2
ECG
150
1/2
ECG
150
1/2
ECG
150
1/3
ECG
75
1/2
ECG
150
4/2
ECG
37
1/4
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECG
150
1/0
ECD
E 15
0 1/
0
ECG
150
3/3
ECG
150
3/3
ECE
225
1/0
ECE
225
1/0
ECG
150
1/0
ECG
150
1/2
ECG
150
1/3
ECG
75
1/2
ECG
150
4/2
ECG
37
1/4
ECG
150
1/0
ECD
450
1/0
ECD
E 15
0 1/
0EC
G 1
50 1
/0EC
G 7
5 1/
0EC
G 1
50 1
/0EC
DE
150
1/0
12.0
313
.14
8.60
5.26
10.6
08.
9014
.06
16.1
026
.40
38.5
02.
221.
482.
302.
422.
311.
602.
69
417
201
292
178
359
302
477
546
895
1305 75 50 78 82 78 54 91
15.0
14.4
8.0
5.5
11.1
8.0
13.4
16.0
25.5
44.0
3.5
2.6
3.5
4.0
6.8
3.5
3.4
0.38
0.37
0.20
0.14
0.28
0.22
0.34
0.41
0.65
1.12
0.09
0.07
0.09
0.10
0.17
0.09
0.09
430
500
500
350
400
350
525
650
950
900
160
120
115
160
105
70 70
430
450
60 60 80 330
500
590
800
900
130
15 100
150
50 70 70
Aero
spac
e, C
onfo
rm, a
nd A
dvan
ced
Com
posi
te F
abric
s (c
ont.)
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,
(664
) 224
-350
6.
34
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
1632
1636
1658
1669
1680
1884
1938
3582
3743
3783
3784
3788
3884
4180
4526
6580
6581
Plai
nPl
ain
Plai
nPl
ain
8H S
atin
8H S
atin
8H S
atin
8H S
atin
4H S
atin
8H S
atin
8H S
atin
12H
Sat
in8H
Sat
in8H
Sat
in2x
2 Ba
sket
8H
Sat
in8H
Sat
in
30 40 20 60 72 44 45 60 49 54 45 42 46 80 36 72 56
32 24 10 12 70 35 36 56 30 48 36 36 36 100
34 72 54
ECG
150
1/0
ECD
E 15
0 1/
0EC
G 1
50 1
/0EC
G 1
50 1
/0EC
DE
150
1/0
ECK
18 1
/0EC
K 18
1/0
ECG
50
1/0
ECG
37
1/0
ECG
37
1/0
ECG
37
1/2
ECG
37
1/2
ECD
E 37
1/2
SCD
450
1/0
SCG
75
1/0
493
SCG
150
1/2
SCG
150
1/2
ECG
75
1/0
ECD
E 15
0 1/
0EC
G 1
50 1
/0EC
D 4
50 1
/0EC
DE
150
1/0
ECK
18 1
/0EC
G 3
7 1/
2EC
G 5
0 1/
0EC
E 22
5 1/
0EC
G 3
7 1/
0EC
G 3
7 1/
2EC
G 3
7 1/
4EC
DE
37 1
/2SC
D 4
50 1
/0SC
G 7
5 1/
0 49
3 SC
G 1
50 1
/2SC
G 1
50 1
/2
3.75
2.60
1.60
2.50
5.70
25.4
026
.76
13.7
08.
4516
.40
26.4
252
.30
26.5
52.
415.
605.
708.
75
127
88 54 85 193
861
907
465
287
556
896
1774
901
82 190
193
297
4.7
4.0
4.0
3.7
6.1
26.0
27.0
14.4
8.5
16.0
25.9
46.7
27.5
3.0
6.0
6.1
10.4
0.12
0.09
0.10
0.09
0.15
0.66
0.69
0.37
0.22
0.41
0.66
1.19
0.70
0.08
0.15
0.15
0.26
150
190
70 300
320
950
880
900
600
550
915
1500
875
75 200
300
400
360
130
70 20 600
800
580
850
60 490
830
1300
740
100
180
250
325
Aero
spac
e, C
onfo
rm, a
nd A
dvan
ced
Com
posi
te F
abric
s (c
ont.)
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.
35
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
6781
6781
(HT)
75
8175
9776
9876
4577
1577
2577
8177
91F
8000
8800
1678
116
791
1764
526
781
8539
2
8H S
atin
8H S
atin
8H S
atin
D
oubl
e Sa
tinC
onfo
rm8H
Sat
in M
odifi
ed P
lain
2/2
Twill
8H S
atin
Con
form
Plai
n4H
Len
o8H
Sat
inC
onfo
rmSa
tinSa
tinPl
ain
57 57 57 30 44 46 80 54 57 58 81 17(8
)58 58 46 56 44
54 57 54 30 32 42 18 18 54 55 8 8 55 55 42 53 30
SCG
75
1/0
SCG
75
1/0
933
ECG
75
1/0
ECG
37
1/4
ECG
75
1/0
ECG
75
1/2
ECG
75
1/0
ECG
75
1/0
ECD
E 75
1/0
ECD
E 75
1/0
ECG
75
1/2
ECG
150
1/0
-EC
G 3
7 1/
3 SC
G 7
5 1/
0SC
G 7
5 1/
0SC
G 7
5 1/
2SC
G 7
5 1/
0SC
G 7
5 1/
0
SCG
75
1/0
SCG
75
1/0
933
ECG
75
1/0
ECG
37
1/4
ECG
75
1/0
ECG
75
1/2
ECG
150
1/0
ECH
25
1/0
ECD
E 75
1/0
ECD
E 75
1/0
Dac
ron
R-1
4EC
G 3
7 1/
3 SC
G 7
5 1/
0SC
G 7
5 1/
0SC
G 7
5 1/
2SC
G 7
5 1/
0T-
5043
8.90
9.00
8.95
38.6
06.
1014
.43
7.30
8.80
8.81
8.95
13.0
98.
259.
009.
0013
.90
8.50
6.00
301
305
303
1309
206
489
248
298
299
303
444
280
305
305
471
288
203
9.0
9.7
9.0
40.6
6.5
13.5
7.7
9.3
8.6
9.0
11.8
16.4
9.5
9.0
13.0
9.0
8.5
0.23
0.25
0.23
1.03
0.17
0.34
0.20
0.24
0.22
0.23
0.30
0.42
0.24
0.23
0.33
0.23
0.21
400
530
300
900
375
560
450
300
570
350
950
290
500
125
700
425
300
325
530
280
800
250
490
80 300
450
300
10 310
350
125
600
350
75
Aero
spac
e, C
onfo
rm, a
nd A
dvan
ced
Com
posi
te F
abric
s (c
ont.)
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.
36
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
1064
1500
1522
1528
1562
1564
1579
1614
1659
1800
2025
2523
2532
3731
3733
3764
4522
Plai
nLe
noPl
ain
Plai
nLe
noPl
ain
Plai
nLe
noLe
noPl
ain
Plai
nPl
ain
Plai
nPl
ain
Plai
nPl
ain
Plai
n
18 20 24 42 30 20 30 30 20 16 20 28 16 17 18 20 24
21 10 22 32 16 18 16 14 10 14 14 20 14 15 18 18 22
ECG
75
1/2
ECG
75
1/3
ECG
150
1/2
ECG
150
1/2
ECG
150
1/0
ECG
37
1/2
ECG
150
1/2
ECG
150
1/0
ECG
150
1/0
ECK
18 1
/0EC
DE
37 1
/3 T
ext
ECH
25
1/0
ECH
25
1/0
ECG
37
1/0
ECG
37
1/0
ECG
37
1/0
SCG
150
1/2
ECG
150
1/2
ECG
37
1/3
ECG
150
1/2
ECG
150
1/2
ECG
150
1/0
ECG
37
1/2
ECG
75
1/0
ECG
75
1/0
ECG
75
1/0
ECK
18 1
/0 E
CD
E 37
1/3
Tex
t EC
H 2
5 1/
0EC
H 2
5 1/
0EC
G 3
7 1/
0EC
G 3
7 1/
0EC
G 3
7 1/
0SC
G 1
50 1
/2
4.68
10.3
03.
675.
971.
8212
.50
3.68
2.33
1.60
9.80
17.1
711
.65
7.25
5.21
5.80
12.0
03.
64
159
349
124
201
62 424
125
79 54 332
582
395
246
177
197
407
123
6.3
25.0
4.8
6.5
4.5
14.0
4.5
5.0
4.2
12.0
26.1
13.0
10.0
5.5
8.0
15.5
5.1
0.16
0.64
0.12
0.17
0.11
0.36
0.11
0.13
0.11
0.30
0.66
0.33
0.25
0.14
0.20
0.39
0.13
220
300
130
250
75 400
120
75 65 330
300
400
300
250
200
250
140
150
310
120
200
50 350
160
85 70 300
225
350
280
200
175
200
125
Fibe
rgla
ss R
einf
orce
d Pl
astic
s (F
RP)
- Bo
at &
Too
ling
Fabr
ics
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.
37
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
4527
4533
4700
4797
4985
6543
6557
7500
7510
7520
7531
7532
7533
7537
7544
7580
7587
Plai
nPl
ain
Plai
nLe
noPl
ain
4H S
atin
4H S
atin
Plai
nPl
ain
Plai
nPl
ain
Plai
nPl
ain
Mod
. Cro
w.
2 En
d Pl
ain
Plai
nM
ock
Leno
24 18 14 28 18 48 57 16 18 18 23 16 18 56 28 24 40
22 18 13 14 22 30 30 14 21 18 14 14 18 25 14 14 20
SC
G 7
5 1/
0 99
3SC
G 7
5 1/
2EC
G 3
7 1/
0EC
G 7
5 1/
0SC
G 7
5 1/
2SC
G 7
5 1/
2SC
G 1
50 1
/2EC
G 3
7 1/
2EC
G 7
5 1/
2EC
G 7
5 1/
3EC
G 7
5 1/
2EC
G 7
5 1/
3EC
G 7
5 1/
2EC
G 7
5 1/
0EC
G 3
7 1/
2EC
G 7
5 1/
2EC
G 3
7 1/
2
SC
G 7
5 1/
0 99
3SC
G 7
5 1/
2EC
DE
75 1
/2EC
G 7
5 1/
2SC
G 1
50 1
/2EC
E 22
5 1/
0EC
E 22
5 1/
0EC
G 3
7 1/
2EC
G 1
50 1
/2EC
G 7
5 1/
3EC
G 7
5 1/
2EC
G 7
5 1/
3EC
G 7
5 1/
2EC
G 3
7 1/
0EC
G 3
7 1/
4EC
G 3
7 1/
0EC
G 3
7 1/
2
3.70
5.92
4.40
4.63
4.70
8.50
5.40
9.60
4.50
8.68
5.50
7.23
5.85
8.50
18.2
06.
2020
.50
125
201
149
157
159
288
183
325
152
294
186
245
198
288
617
210
695
4.0
7.4
4.7
7.4
6.2
9.1
5.8
11.0
7.0
12.0
9.0
10.0
8.0
8.5
20.0
7.8
30.0
0.10
0.19
0.14
0.19
0.16
0.23
0.15
0.28
0.18
0.30
0.23
0.25
0.20
0.22
0.51
0.20
0.76
140
270
160
170
320
600
350
300
125
330
160
250
220
225
500
310
750
130
300
150
170
170
60 60 250
75 330
110
200
220
175
500
280
450
Fibe
rgla
ss R
einf
orce
d Pl
astic
s (F
RP)
- Bo
at &
Too
ling
Fabr
ics
(con
t.)
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.
38
39
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
Wei
ght
P
erm
iabi
lity
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(i
n)
W
arp
F
ill2
2
417
419
601
602
647
651
3602
3626
3635
3636
7574
7576
Cro
wfo
ot3x
1 Tw
ill3x
1 Tw
ill3x
1 Tw
illM
od T
will
3x1
Twill
3x1
Twill
3x1
Twill
Mod
Tw
ill3x
1 Tw
illSp
ecia
lSp
ecia
l
54 53 54 53 47TO
P BE
AM44 54 48 44 44 48 48
52 54 30 30 30 24 30 24 22 22 40 40
ECD
E 75
1/0
ECD
E 75
1/0
ECD
E 15
0 1/
2EC
DE
150
1/2
EC
DE
37 1
/0 +
ECD
E 37
1/0
Tex
tEC
DE
37 1
/0
ECD
E 75
1/0
ECD
E 37
1/0
ECD
E 37
1/0
ECD
E 37
1/0
ECD
E 75
1/2
ECD
E 75
1/2
ECD
E 75
1/0
ECD
E 75
1/0
ECD
E 15
0 1/
4 Te
xtEC
DE
75 1
/2 T
ext
DE
75 1
/0x3
Tex
t
ECD
E 75
1/0
+EC
DE
75 1
/2 T
ext
ECD
E 15
0 1/
0 +
ECD
E 50
1/0
Tex
t EC
DE
75 1
/3 T
ext
ECD
E 75
1/4
Tex
t EC
DE
75 1
/4 T
ext
ECD
E 75
1/0
x2 T
ext
ECD
E 75
1/0
x4 T
ext
8.30
8.40
9.25
9.50
15.3
0
13.0
0
8.90
13.4
014
.50
14.5
016
.50
21.5
0
281
284
313
322
518
440
301
454
491
491
559
728
8-18
35-5
560
-90
75-1
1025
-50
60-9
0
65-9
5
45-8
050
-80
45-8
080
-120
40-8
0
375
350
320
325
350
575
350
550
500
550
500
325
325
120
100
325
350
225
200
250
250
500
Filtr
atio
n Fa
bric
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
Fi
nish
Lo
ss o
n P
erm
iabi
lity
M
ulle
n
Wei
ght
MIT
Fle
x (A
fter A
cid)
St
reng
th (l
bf/in
)
Igni
tion
(in
)
Burs
t
(oz/
yd )
(g/m
)
W
arp
F
ill
W
arp
F
ill2
2
647
651
651
651
651
651
3602
3602
3602
3602
3602
7576
7576
7576
7576
7576
Teflo
n B
Trite
mp
Teflo
n B
Ultr
a-Fl
exAc
id-F
lex
162
5-Ac
id R
esis
t T
ritem
p T
eflo
n B
Ultr
a-Fl
exAc
id-F
lex
162
5-Ac
id R
esis
tTr
item
p T
eflo
n B
Ultr
a-Fl
exAc
id-F
lex
162
5 Ac
id R
esis
t
10.0
min
.1.
7 m
in.
10.0
min
.7.
0 m
in.
5.0
min
.5.
0 m
in.
1.7
min
.10
.0 m
in.
7.0
min
.7.
0 m
in.
5.0
min
1.7
min
.10
.0 m
in.
7.0
min
.5.
0 m
in.
10 m
in.
25-5
535
-65
30-6
035
-60
25-6
535
-60
40-6
030
-60
25-6
025
-60
35-6
025
-55
25-6
020
-50
15-5
030
-90
600
600
600
600
500
600
500
500
500
500
500
800
500
800
800
800
15.8
-17.
8 13
.50
14.0
012
.9-1
4.4
14.0
012
.9-1
4.2
9.00
10.0
09.
509.
508.
9-10
.021
.00
22.4
022
.00
21.8
021
.5-2
5.7
535-
603
457
474
437-
487
474
437-
480
305
339
322
322
302-
33.9
711
758
745
738
728-
871
- - -16
k+
10k+ - - -
20k+
15k+ - - -
18k+
9k+ -
300
450
650
500
400
650
250
325
250
250
350
350
650
500
550
600
250
200
300
250
200
300
175
200
175
175
250
300
450
350
500
500
- - -20
0k+
100k
+- - -
200k
+10
0k+
- - -10
0k+
80k+ -
Filtr
atio
n Fi
nish
ed 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.
40
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
332
333
1523
1629
1633
1636
1658
1692
1694
1695
1908
3713
7628
1
4H S
atin
4H S
atin
Plai
nPl
ain
Plai
nPl
ain
Plai
nPl
ain
Plai
nPl
ain
Mod
Tw
illPl
ain
Satin
48 49 28 13 40 40 20 40 40 40 32 13 44
32 32 20 9 20 24 10 20 24 24 15 12 32
ECG
37
1/0
ECD
E 37
1/0
ECG
150
3/2
ECG
75
1/0
ECG
150
1/0
ECD
E 15
0 1/
0EC
G 1
50 1
/0EC
G 1
50 1
/0EC
G 1
50 1
/0EC
DE
150
1/0
ECD
E 37
3x
ECG
37
1/3
ECG
75
1/0
ECG
37
1/0
ECD
E 37
1/0
ECG
150
3/2
ECG
75
1/0
ECG
75
1/0
ECD
E 15
0 1/
0EC
G 7
5 1/
0EC
G 7
5 1/
0EC
G 7
5 1/
0EC
DE
75 1
/0EC
DE
11.6
Tex
tEC
G 3
7 1/
3EC
G 7
5 1/
0
12.6
012
.78
11.5
01.
783.
202.
611.
603.
393.
543.
5924
.011
.70
6.00
427
433
390
60 108
88 54 115
120
122
812
396
203
13.5
13.8
13.0
4.9
4.1
3.7
4.0
4.6
4.9
5.4
40.0
14.5
7.0
0.34
0.35
0.33
0.13
0.11
0.09
0.10
0.12
0.13
0.14
1.02
0.37
0.18
550
660
450
125
190
70 170
200
190
600
400
300
400
490
300
75 130
70 180
220
180
250
325
200
Insu
latio
n C
oatin
g Fa
bric
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.
41
Styl
e W
eave
Fin
ish
Cou
nt
Cou
nt
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
War
p
Fill
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
1908
*19
1620
2320
2520
2520
2520
2520
35*
2035
*84
215
8421
584
215
8421
784
217
8421
784
220
8422
484
225
8422
6
Mod
Tw
illPl
ain
Plai
nPl
ain
Plai
nPl
ain
Plai
nM
od T
will
Mod
Tw
illPl
ain
Plai
nPl
ain
Mod
Pla
inM
od P
lain
Mod
Pla
inTw
illG
Fill
G F
illG
Ffil
l
32 20 20 20 20 20 20 20 20 18 18 18 18 18 18 18 18 18 18
16 13 9 14 14 14 14 14 14 14 14 14 14 14 14 16 15 15 15
24.0
017
.00
26.0
017
.70
17.7
017
.70
17.7
033
.00
33.0
08.
508.
5014
.50
8.50
8.50
14.5
023
.00
7.90
8.00
8.00
812
575
880
599
599
599
599
1117
1117
288
288
491
288
288
491
779
267
271
271
40.0
24.0
40.0
26.0
23.0
25.0
40.0
56.0
58.0
16.5
14.0
26.0
16.0
14.0
35.0
33.0
15.5
13.5
13.4
1.02
0.61
1.02
0.66
0.58
0.64
1.02
1.42
1.47
0.42
0.36
0.66
0.41
0.36
0.89
0.84
0.39
0.34
0.34
600
400
400
300
300
300
350
300
300
175
175
175
175
150
150
550
175
200
200
250
200
300
150
150
150
200
450
450
100
100
100
100
100
100
450
100
150
150
9383
Gre
ige
9383
9383
9957
9987
9480
9383
9752
9383
9957
9995
9383
9957
9995
Gre
ige
9383
9383
9383
Insu
latio
n G
lasT
ex F
abric
s
* Not
cov
ered
by
MIL
-C-2
0079
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.
42
S
tyle
W
idth
Le
ngth
Wei
ght
Th
ickn
ess
R
olls
/Car
ton
Car
tons
/Pal
let
Stre
ngth
(lbf
/in)
(
in)
(
in)
(oz
/yd
) (g
/m )
(mils
) (
mm
)
War
p
Fill
22
1350
1351
1352
1353
1358
1362
9.5/
38/4
8/72
38/4
838
/48
38/4
838
/48
38/4
8
50 (a
ll)50 25 50 25 25
4.30
5.50
11.5
04.
8014
.00
20.5
0
145.
618
6.2
389.
316
2.5
473.
969
3.9
14.0
29.0
22.0
31.0
55.0
0.36
0.74
0.56
0.79
1.40
140
150
300
325
750
170
250
400
650
550
16/4
/24 4 200 4 2
9/9/
9/12
9 9 240 9 9/6
EIFS
Mes
h Fa
bric
s
The
phys
ical
pro
perti
es li
sted
are
app
roxi
mat
e gu
ides
onl
y. Ac
tual
val
ues
may
var
y. Fo
r add
ition
al in
form
atio
n, p
leas
e co
ntac
t aTe
chni
cal S
ervi
ce R
epre
sent
ativ
e, (8
64) 2
24-3
506.
Alka
li R
esis
tant
Fin
ishe
d Fa
bric
s
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
W
arp
F
ill
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
22
1350
1351
1352
1353
1358
1362
Leno
Leno
Leno
Leno
Leno
Leno
12 12 16 6 16 12
6 6 6 3 3 3
3700
yd/
lb37
00 y
d/lb
1800
yd/
lb18
00 y
d/lb
1800
yd/
lb45
0 yd
/lb
1800
yd/
lb12
00 y
d/lb
650
yd/lb
900
yd/lb
225
yd/lb
225
yd/lb
3.90
4.50
9.20
4.00
13.0
019
.00
132.
015
2.3
311.
413
5.4
440.
164
3.2
8.0
15.0
20.0
15.0
30.0
50.0
0.20
0.38
0.51
0.38
0.76
1.27
Gre
ige
or U
nfin
ishe
d Fa
bric
s
43
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
(o
z/yd
) (g
/m )
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)2
22
22
22
22
2
Fibe
rgla
ss F
abric
Wei
ght I
ndex
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
Tec
hnic
al
Serv
ice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
101
104
1071
1037
993
106
1297
1035
1067
APS
1067
1299
1070
1065
6060
1080
108
1078
0.48
0.55
0.60
0.68
0.71
0.72
0.82
0.88
0.88
0.91
0.92
1.01
1.08
1.15
1.38
1.40
1.41
16 19 20 23 24 24 27 30 30 31 31 34 37 39 47 48 48
1180
1609
1280
APS
1280
3080
1620
1076
1658
1659
1081
1629
1562
2112
112
1608
1610
2113
1.44
1.48
1.54
1.55
1.57
1.58
1.60
1.60
1.60
1.72
1.78
1.82
2.04
2.08
2.22
2.30
2.30
49 50 53 53 53 54 54 54 54 59 60 62 69 71 75 78 78
78 79 81 81 81 81 81 82 82 85 88 88 88 90 90 91 91
2875
119
2319
3070
1674
1675
2116
116
3116
1634
2316
1677
120
1316
2117
1633
1678
2.70
2.71
2.72
2.74
2.82
2.84
3.06
3.09
3.10
3.11
3.13
3.15
3.16
3.18
3.18
3.20
3.20
92 92 92 93 97 97 104
105
105
105
106
106
111
107
108
108
108
1617
1614
113
139
117
2313
3313
4180
1611
1669
2154
1636
1636
1125
2119
1628
2114
2.31
2.33
2.39
2.39
2.40
2.40
2.40
2.41
2.42
2.50
2.54
2.60
2.61
2.65
2.66
2.69
2.69
220
1692
1634
1694
1647
2165
1165
1695
4522
1131
1522
1579
4527
1632
1167
1161
1165
3.22
3.39
3.50
3.54
3.55
3.55
3.57
3.59
3.64
3.65
3.67
3.68
3.70
3.75
3.82
3.87
4.00
109
115
118
122
122
122
122
122
123
124
124
125
125
127
129
131
136
44
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
(o
z/yd
) (g
/m )
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)2
22
22
22
22
2
Fibe
rgla
ss F
abric
Wei
ght I
ndex
(con
t.)
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
Tec
hnic
al
Serv
ice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
1649
1676
1652
1141
1350
1651
1503
1504
2157
4700
7510
2166
4797
1064
7660
1502
4985
4.01
4.06
4.09
4.20
4.30
4.31
4.36
4.36
4.36
4.40
4.50
4.60
4.63
4.68
4.73
4.78
4.85
136
138
138
142
146
146
148
148
148
149
152
155
157
159
160
162
159
163
164
164
165
168
171
177
178
181
183
183
184
186
186
186
190
193
1680
6580
3733
7533
1538
7627
4533
1528
7255
7628
7628
185
392
7698
7650
7629
7580
7629
0
5.70
5.70
5.80
5.85
5.87
5.87
5.92
5.94
6.00
6.00
6.00
6.00
6.10
6.12
6.19
6.20
6.27
193
193
197
198
199
199
201
201
203
203
203
203
206
208
210
210
213
1353
1500
7630
1501
7618
1047
3731
1557
1526
6557
7626
1047
1351
7531
7624
4526
880
4.80
4.83
4.84
4.86
4.95
5.10
5.21
5.26
5.33
5.40
5.40
5.44
5.50
5.50
5.50
5.60
5.70
139
1528
7667
138
7642
7637
7642
7635
7637
7635
7532
7715
7640
7652
8800
417
1142
6.50
6.50
6.54
6.66
6.72
6.73
6.84
6.85
7.08
7.09
7.23
7.30
7.60
7.60
8.25
8.30
8.37
220
220
222
226
228
228
232
232
240
240
245
248
258
258
280
281
285
419
403
3743
6543
7537
2678
115
4375
2052
036
0165
8115
8177
2577
8136
0267
8175
81
8.40
8.40
8.45
8.50
8.50
8.50
8.60
8.68
8.70
8.75
8.75
8.80
8.81
8.90
8.90
8.90
8.95
285
285
287
288
288
288
292
294
295
297
297
298
299
301
301
301
303
45
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
Sty
le
Wei
ght
(o
z/yd
) (g
/m )
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)
(oz/
yd )
(g/m
)2
22
22
22
22
2
303
305
305
305
313
322
325
328
332
332
349
359
390
390
395
396
407
3764
1527
6045
1564
232
332
1163
333
653
651
8000
1530
1530
1582
3626
3582
1764
5
12.0
012
.03
12.2
512
.50
12.6
012
.60
12.6
312
.78
12.8
613
.00
13.0
913
.14
13.2
013
.20
13.4
013
.70
13.9
0
407
417
415
424
427
427
428
433
435
441
444
445
448
448
454
465
471
7791
678
1(H
T)16
781
1679
160
160
275
0033
418
0015
0715
00*
1576
1352
1523
2523
3713
162
8.95
9.00
9.00
9.00
9.25
9.50
9.60
9.70
9.80
9.80
10.3
010
.60
11.5
011
.50
11.6
511
.70
12.0
1
1358
7645
3635
3636
634
1527
647
1583
3783
2025
7544
1362
7587
7576
1908
1884
1584
14.0
014
.43
14.5
014
.50
15.0
015
.00
15.3
016
.10
16.4
017
.17
18.2
020
.50
20.5
021
.50
24.0
025
.40
26.4
0
474
489
491
491
508
508
518
546
556
582
610
695
695
728
812
861
895
3784
3884
1938
1597
7597
3788
26.4
226
.55
26.7
638
.50
38.6
052
.30
896
901
907
1305
1309
1774
Fibe
rgla
ss F
abric
Wei
ght I
ndex
(con
t.)
The
phys
ical
pro
perti
es li
sted
are
for g
reig
e (u
ntre
ated
) fab
rics.
Act
ual v
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s m
ay v
ary.
For a
dditi
onal
info
rmat
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ple
ase
cont
act
a Te
chni
cal S
ervi
ce R
epre
sent
ativ
e, (8
64) 2
24-3
506.
*1
500
Leno
46
Sty
le
Thic
knes
s
St
yle
T
hick
ness
S
tyle
T
hick
ness
S
tyle
T
hick
ness
S
tyle
T
hick
ness
(mils
) (m
m)
(m
ils)
(mm
) (m
ils)
(mm
)
(mils
) (m
m)
(mils
) (m
m)
101
104
1035
1037
993
1071
106
106
7 AP
S10
6710
7810
7060
6010
65 1
280
APS
1080
1280
1299
1.0
1.1
1.1
1.1
1.2
1.2
1.3
1.3
1.4
1.7
1.8
1.9
2.1
2.1
2.1
2.2
2.3
0.02
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.04
0.04
0.05
0.05
0.05
0.05
0.05
0.06
0.06
1180
1297
3080
108
1081
117
1609
3132
1076
4180
2113
2112
2114
3113
3313
113
1628
2.3
2.3
2.3
2.4
2.4
2.6
2.6
2.8
2.9
3.0
3.1
3.2
3.2
3.2
3.3
3.4
3.4
0.06
0.06
0.06
0.06
0.06
0.07
0.07
0.07
0.07
0.08
0.08
0.08
0.08
0.08
0.08
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
0.09
1677
2116
2117
1674
2316
116
1165
1316
1611
1636
1658
1675
2165
4527
1633
1647
1649
3.7
3.7
3.7
3.8
3.8
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.1
4.1
4.1
0.09
0.09
0.09
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.11
0.11
0.11
2119
2319
3070
3323
120
220
1608
1610
1620
3116
112
1125
119
2125
1634
1636
1669
3.4
3.4
3.4
3.4
3.5
3.5
3.5
3.5
3.5
3.5
3.6
3.6
3.6
3.6
3.7
3.7
3.7
1659
1678
1167
1562
1579
1652
2875
1692
1632
4700
1161
1522
1634
1676
1504
1629
1694
4.2
4.3
4.4
4.5
4.5
4.5
4.5
4.6
4.7
4.7
4.8
4.8
4.8
4.8
4.9
4.9
4.9
0.11
0.11
0.11
0.11
0.11
0.11
0.11
0.12
0.12
0.12
0.12
0.12
0.12
0.12
0.13
0.13
0.13
Fibe
rgla
ss F
abric
Thi
ckne
ss In
dex
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
Tec
hnic
al
Serv
ice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
47
Sty
le
Thic
knes
s
St
yle
T
hick
ness
S
tyle
T
hick
ness
S
tyle
T
hick
ness
S
tyle
T
hick
ness
(mils
) (m
m)
(m
ils)
(mm
) (m
ils)
(mm
)
(mils
) (m
m)
(mils
) (m
m)
1131
1614
2157
4522
1503
1651
1695
1557
2166
3731
1501
1044
1047
6557
1500
1502
1526
5.0
5.0
5.1
5.1
5.3
5.3
5.4
5.5
5.5
5.5
5.5
5.6
5.8
5.8
5.9
5.9
5.9
0.13
0.13
0.13
0.13
0.13
0.14
0.14
0.14
0.14
0.14
0.14
0.14
0.15
0.15
0.15
0.15
0.15
7660
880
4526
7626
7630
1680
6580
4985
1064
7624
139
1528
7618
7627
7698
138
1617
5.9
6.0
6.0
6.0
6.0
6.1
6.1
6.2
6.3
6.4
6.5
6.5
6.5
6.5
6.5
6.6
6.8
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.16
0.16
0.16
0.17
0.17
0.17
0.17
0.17
0.17
0.17
0.17
0.18
0.18
0.18
0.18
0.18
0.18
0.18
0.19
0.19
0.19
0.19
0.20
0.20
0.20
0.20
0.20
1581
3733
7652
3743
7537
8539
277
8176
3740
367
8175
3175
8116
791
2678
177
91F
520
6543
8.0
8.0
8.3
8.5
8.5
8.5
8.6
8.8
8.9
9.0
9.0
9.0
9.0
9.0
9.0
9.1
9.1
0.20
0.20
0.21
0.22
0.22
0.22
0.22
0.22
0.23
0.23
0.23
0.23
0.23
0.23
0.23
0.23
0.23
7628
1141
7255
7510
7628
176
290
1538
7629
7669
4533
4797
7650
7715
7580
7196
7635
1543
6.8
7.0
7.0
7.0
7.0
7.0
7.0
7.1
7.2
7.4
7.4
7.5
7.7
7.8
7.9
7.9
8.0
7725
1678
176
37 67
81 (H
T)76
4033
425
3275
3276
4265
8175
0076
4211
4215
7611
8880
0075
20
9.3
9.5
9.6
9.7
9.8
10.0
10.0
10.0
10.0
10.4
11.0
11.0
11.1
11.1
11.8
11.8
12.0
0.24
0.24
0.24
0.25
0.25
0.25
0.25
0.25
0.25
0.26
0.28
0.28
0.28
0.28
0.30
0.30
0.30
Fibe
rgla
ss F
abric
Thi
ckne
ss In
dex
(con
t.)
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
Tec
hnic
al
Serv
ice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
48
Sty
le
Thic
knes
s
St
yle
T
hick
ness
S
tyle
T
hick
ness
S
tyle
T
hick
ness
S
tyle
T
hick
ness
(mils
) (m
m)
(m
ils)
(mm
) (m
ils)
(mm
)
(mils
) (m
m)
(mils
) (m
m)
1523
2523
1764
515
8233
276
4516
233
313
5015
6415
3035
8223
237
1315
2737
6415
83
13.0
13.0
13.0
13.4
13.5
13.5
13.8
13.8
14.0
14.0
14.4
14.4
14.6
14.5
15.0
16.0
16.0
0.33
0.33
0.33
0.34
0.34
0.34
0.35
0.35
0.36
0.36
0.37
0.37
0.37
0.37
0.38
0.41
0.41
3783
8800
7544
1353
1500
*15
0715
8437
8418
8420
2519
3875
8738
8413
5213
5819
0875
97
16.0
16.4
20.0
22.0
25.0
25.0
25.5
25.9
26.0
26.1
27.0
27.2
27.5
29.0
31.0
40.0
40.6
0.41
0.42
0.51
0.56
0.56
0.65
0.65
0.66
0.66
0.66
0.69
0.69
0.70
0.74
0.79
1.02
1.03
1.12
1.24
1.40
1597
3788
1362
44.0
48.7
55.0
Fibe
rgla
ss F
abric
Thi
ckne
ss In
dex
(con
t.)
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
Tec
hnic
al
Serv
ice
Rep
rese
ntat
ive,
(864
) 224
-350
6.
*
1500
Len
o
49
ASTROQUARTZ ® PRODUCTS*Astroquartz ® is a registered trademark of JPS Industries
Astroquartz ® II &Astroquartz III ® PropertiesAstroquartz II ® and original Astroquartz are composed of identical raw materials. Through improved manufacturing and handling technologies Astroquartz II represents a stronger,cleaner product 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
1010
10
50
Physical Properties of Fused Quartz (cont.)
OpticalRefractive Index @ 15ºC...............................................1.4585Dispersion............................................................................ 67Field of Transparency (µm)....................................... 0.2 to 4.0
Astroquartz ® ApplicationsAstroquartz ® fabrics offer better solutions to high heat, highstrength problems.
The aerospace industry relies on Astroquarz fiber productsmade from pure fused silica (99.99% SiO ). An outstandingreinforcement for high temperature and ablative space andmissile applications. Astroquartz products are recommended when low dielectric loss properties are required, such as microwave transmission in radome and antenna applications.
Other applications include insulation for the space shuttle,cable tray insulation for nuclear power plants, and laminatedfabric for circuit boards.
Conform formable Astroquartz fabrics are recommended for use in preforms for resin transfer molding (RTM), pressmolding, and tooling applications.
Design Considerations for Astroquartz ® Fabric SelectionThere 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.
2
51
Design Considerations for Astroquartz ® Fabric Selection (cont.)ConstructionThis is determined by the number of warp yarns/denier (in themachine direction) and filling yarns/denier (in the cross-machine direction) per inch of the fabric.
Yarn SizeYarn size determines the weight and thickness of the fabric.For specific applications, one yarn may be selected over another to take advantage of the fabric’s performancecharacteristics.
FinishMost industrial applications require that Astroquartz fabric beused along with another material. For compatibility a finish or after treatment is often applied to the fabric.
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.
Finish Matrix PerformanceCode Resin Features
S-928 Epoxy Epoxy functional silane.
933 HTS Polyimide, Epoxy, Excellent high temperature Bismaleimide and moisture resistance.
S-977 Epoxy, Melamine, Applied to scoured fabric Phenolic, PE for superior bonding strength.
1059 HT/ Polyimides, Recommended for high2059 HT/ Thermoplastic temperature (700ºF) systems.3059 HT Matrices
9779 Epoxy, High performance amino- Bismaleimide silane yarn binder, applied to yarn for woven fabric.
52
Astroquartz ® II & III Fabric Finishes (cont.) Finish Matrix PerformanceCode Resin Features
9827/ Epoxy, Polyimide, Applied to scoured fabrics.2827/ Bismaleimide Recommended for electronic3827 and aerospace applications.
9836/ Epoxy, 9779 finished fabric is washed2836/ Bismaleimide to remove nonfunctional3836 organic binder components.
9837/ Polyester, Applied to scoured fabrics.2837/ Vinyl Ester Recommended for resins 3837 cured by vinyl addition.
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 choppedfrom 1/8” to 1” fiber with 9779 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.
253
S
tyle
W
eave
Cou
nt C
ount
W
arp
F
ill
W
eigh
t
Thi
ckne
ss
Stre
ngth
(lbf
/in)
W
arp
F
ill
Ya
rn
Ya
rn
(oz
/yd
) (g
/m )
(m
ils)
(m
m)
War
p
Fill
22
503
507
525
527
531
533
557
570
572
581
591
593
594
4503
4581
Plai
nPl
ain
Plai
nPl
ain
8H S
atin
2x2
Bask
etC
row
foot
5H S
atin
Plai
n8H
Sat
inC
onfo
rm5H
Sat
inLe
noPl
ain
8H S
atin
50 27 50 42 68 36 57 38 17 57 57 49 20 40 47
40 25 50 32 65 36 31 24 16 54 54 46 10 31 44
QC
G 3
00 1
/2Q
CG
300
1/2
QC
G 3
00 1
/0Q
CG
300
2/2
QC
G 3
00 1
/2Q
CG
300
2/2
QC
G 3
00 2
/2Q
CG
300
2/8
QC
G 3
00 2
/8Q
CG
300
2/2
QC
G 3
00 2
/2Q
CG
300
2/2
QC
G 3
00 2
/2Q
CK
125
1/0
QC
K 12
5 2/
0
QC
G 3
00 1
/2Q
CG
300
1/2
QC
G 3
00 1
/0Q
CG
300
2/2
QC
G 3
00 1
/2Q
CG
300
2/2
QC
G 3
00 2
/2Q
CG
300
2/8
QC
G 3
00 2
/8Q
CG
300
2/2
QC
G 3
00 2
/2Q
CG
300
2/2
QC
G 3
00 2
/2Q
CK
125
1/0
QC
K 12
5 2/
0
3.58
2.10
2.00
6.10
5.20
5.30
5.00
19.5
9.90
8.60
8.45
7.50
2.40
3.38
8.45
128
71 68 206
176
179
169
659
335
291
286
254
81 114
286
5.0
4.0
3.0
8.0
7.0
7.0
6.0
27.0
17.0
10.0
12.0
9.0
8.0
5.0
10.0
0.13
0.10
0.08
0.20
0.18
0.18
0.15
0.69
0.43
0.25
0.30
0.23
0.20
0.13
0.25
155
80 65 270
225
250
410
825
590
400
420
270
90 115
370
140
60 65 250
200
250
55 650
480
375
350
270
55 100
330
Astro
quar
tz ®
II &
III 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
Tec
hnic
al S
ervi
ce
Rep
rese
ntat
ive,
(864
) 224
-350
6. N
ote:
AQ
II fa
bric
s ar
e w
oven
with
977
9 re
sin
com
patib
le b
inde
r. AQ
III a
re a
vaila
ble
only
as
finis
hed
fabr
ics.
54
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.)
BinderAstroquartz s/550 mat is impregnated with a polyvinyl alcoholbinder in the manufacturing operation. This provides a stablemat 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-2343 ** Test Method - ASTM D-578• +0-1 •• ±10% † Tensile, min. avg., determined on uncoated roving
22
33
2
2
3
55
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.
Because of its high strength and flexibility, high purity andhigh temperature resistance, Astroquartz II sewing thread is widely used in sewing or wrapping insulation blankets, shrouds, blast curtains and separators.
The strength, smoothness and flexibility of Astroquartz IIsewing threads are far superior to any quartz threads previously offered.
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
56
Astroquartz ® II YarnAstroquartz ® II 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 II yarn has a higher tensile strength andabrasion resistance. As a result, high production efficienciesare now possible in the production of high temperatureflexible insulation.
Astroquartz II 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 II yarns are available with the 9779 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 Characteristics*Astroquartz II Astroquartz IIINumber of Filaments300 1/0 - 120 filaments 125 1/0 - 120 filaments300 2/0 - 240 filaments 125 2/0 - 240 filaments300 2/2 - 480 filaments * Each filament is 9 µm in diameter, equivalent to a fiberglass “G” filament.
57
Astroquartz ® II 350ºF Epoxy LaminatesStyle 581-9779/CE-900 Epoxy Prepreg*Property Results**Tensile Strength, Room Temperature........................ 715 MPaTensile Strength, 1/2 Hour @ 350ºF.......................... 635 MPaYoung’s Modulus, Room Temperature......................... 28 GPaYoung’s Modulus, 1/2 Hour @ 350ºF........................... 25 GPa
Flexural Strength, Room Temperature....................... 682 MPaFlexural Strength, 1/2 Hour @ 350ºF......................... 523 MPaTaylor’s Modulus, Room Temperature......................... 24 GPaTaylor’s Modulus, 1/2 Hour @ 350ºF............................21 GPa
Compressive Strength, Room Temperature...............499 MPaCompressive Strength, 1/2 Hour @ 350ºF.................344 MPaCompressive Modulus, Room Temperature................. 26 GPaCompressive Modulus, 1/2 Hour 2 350ºF.....................23 GPa* Cytec Corporation ** Average of 3 runs, 32 wt% resin content, 1.77 g/cm specific gravity
Astroquartz ® II Toughened Epoxy Laminates Style 581/R7376 Prepreg*Property Results**Flexural Strength, Room Temperature.......................889 MPaFlexural Strength, 180ºF............................................ 770 MPaTaylor’s Modulus, Room Temperature......................... 28 GPaTaylor’s Modulus, 180ºF............................................... 27 GPa
Compressive Strength, Room Temperature...............608 MPaCompressive Strength, 180ºF.................................... 534 MPaCompressive Modulus, Room Temperature................. 29 GPaCompressive Modulus, 180ºF...................................... 26 GPa
Short Beam Shear Strength, Room Temperature........ 91 MPaShort Beam Shear Strength, 180ºF..............................81 MPa* Cytec Corporation ** 32 wt% resin content, 0.009 in. ply thickness
58
Astroquartz ® II Polyimide LaminatesStyle 581-9779/F-178 Polyimide Prepreg*Property Results**Tensile Strength, Room Temperature........................ 726 MPaYoung’s Modulus, Room Temperature......................... 27 GPa
Flexural Strength, Room Temperature.......................701 MPaFlexural Strength, 1/2 Hour @ 350ºF......................... 471 MPaTaylor’s Modulus, Room Temperature......................... 22 GPaTaylor’s Modulus, 1/2 Hour @ 350ºF............................18 GPa
Compressive Strength, Room Temperature...............462 MPaCompressive Strength, 1/2 Hour @ 350ºF.................266 MPaCompressive Modulus, Room Temperature................. 26 GPaCompressive Modulus, 1/2 Hour 2 350ºF.....................19 GPa* Hexcel Corporation ** 36.2 wt% resin content
Astroquartz ® II Lightweight 8-Harness Satin Fabric Style 531-9827/EPON 828 Prepreg*Nadic Methyl Anhydride Wet LayupProperty Results**Tensile Strength, Room Temperature.......................... 64 MPa
Flexural Strength, Room Temperature.......................818 MPaTaylor’s Modulus, Room Temperature......................... 25 GPa
Compressive Strength, Room Temperature...............580 MPa* Shell Chemical Company** 20 Plies, 34.2 wt% resin content, 0.0062” ply thickness
Astroquartz ® II RovingImpregnated Strand Test, ASTM D-2343*Property ResultsAstroquartz II-9779......................................................3.7 GPa“S-2” Fiberglass-463................................................... 3.6 GPa“S” Fiberglass-901...................................................... 3.8 GPa“E” Fiberglass-456.......................................................1.9 GPa“E” Fiberglass-462.......................................................1.9 GPa* Owens Corning Fiberglass Corporation Pub No. 5-ASP 10139-A
59
Astroquartz ® II Unidirectional FabricStyle 557-9779/EPON 828*/Eporal/BF3 Wet LayupProperty Results**Tensile Strength, Room Temperature..........................1.1 GPaTensile Strength, 2 Hour Boil.......................................1.0 GPaFlexural Strength, Room Temperature........................ 1.1 GPaFlexural Strength, 2 Hour Boil..................................... 1.1 GPaTaylor’s Modulus, Room Temperature..........................35 GPaTaylor’s Modulus, 2 Hour Boil.......................................35 GPa
Compressive Strength, Room Temperature...............657 MPaCompressive Strength, 2 Hour Boil............................604 MPa* Shell Chemical Company ** 33.6 wt% resin content, 12 Plies, 0.066” Thickness
Astroquartz ® II Dielectric Properties Typical Dielectric Properties of Astroquartz II
Quartz/Polyimide Compared to E-glass/Polyimide, 9.4 GHz Dielectric Loss Constant, Dk Tangent, DfTemperature % Resin AQ II E-glass AQ II E-glass Room 35 3.30 3.87 0.005 0.009600ºF 35 3.25 4.20 0.003 0.009
Quartz/Silicone Compared to E-glass/Silicone, 9.4 GHz Dk DfTemperature % Resin AQ II E-glass AQ II E-glass Room - 3.21 4.35 0.003 0.006500ºF - 3.21 4.31 0.003 0.006
Quartz/Polybutadiene versus E-glass/Polybutadiene, 35GHz* Dk DfTemperature % Resin AQ II E-glass AQ II E-glass Room - 3.10 4.20 0.003 0.010* Fibercote Industries, AQ II s/581-910, E-glass s/7781-550
Dielectric Properties of Various Glasses, 9.4GHz Dk DfTemp. AQ II E-glass S-glass AQ II E-glass S-glass Room 3.78 6.13 5.21 0.0001 0.004 0.007
60
Astroquartz ® III Plain Weave FabricStyle 4503-9836/EPON 828 Prepreg*Nadic Methyl Anhydride Wet LayupProperty Results**Tensile Strength, Room Temperature........................ 674 MPaTensile Strength, 2 Hour Boil..................................... 651 MPa
Flexural Strength, Room Temperature.......................653 MPaFlexural Strength, 2 Hour Boil.................................... 619 MPaTaylor’s Modulus, Room Temperature..........................21 GPaTaylor’s Modulus, 2 Hour Boil.......................................21 GPa
Compressive Strength, Room Temperature...............455 MPaCompressive Strength, 2 Hour Boil............................443 MPa
Specific Gravity........................................................1.78 g/cm* Shell Chemical Company ** 12 Plies, 40.7 wt% resin content, 0.121” laminate thickness
Astroquartz ® III 8-Harness Satin Fabric Style 4581-9836/EPON 828 Laminate*Nadic Methyl Anhydride Wet LayupProperty Results**Tensile Strength, Room Temperature........................ 707 MPaTensile Strength, 2 Hour Boil..................................... 667 MPa
Flexural Strength, Room Temperature.......................819 MPaFlexural Strength, 2 Hour Boil....................................793 MPaTaylor’s Modulus, Room Temperature......................... 23 GPaTaylor’s Modulus, 2 Hour Boil...................................... 24 GPa
Compressive Strength, Room Temperature...............558 MPaCompressive Strength, 2 Hour Boil............................546 MPa
Specific Gravity........................................................1.82 g/cm* Shell Chemical Company ** 12 Plies, 35.1 wt% resin content, 0.123” laminate thickness
3
3
61
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.
62
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
TexThe 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.
63
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.
Finish PerformanceCode Features
CS-811 Loom state fabric
CS-800 Scour finish for Aramid fabrics
CS-802 Scour finish for Spectra ® and Dyneema ® fabrics
CS-892 Water repellent finish for Spectra ® and Dyneema ®* fabrics
CS-897 Water repellent finish for Aramid fabrics
CS-898 Proprietary finish for Kevlar ® fabrics
CS-899 Proprietary finish for Twaron ® fabrics
LCS Laminated Composite Substrate
ML Micro-Laminate
WRT Water Repellent Treated
64
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775
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1100
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980
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760
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1200
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930
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960
775
Kevl
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29,
129
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s
The
phys
ical
pro
perti
es li
sted
are
for g
reig
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ntre
ated
) fab
rics.
Act
ual v
alue
s m
ay v
ary.
JPSC
M s
trong
ly re
com
men
ds d
esig
ners
and
use
rs p
erfo
rm
test
ing
for a
pplic
atio
n an
d pa
ckag
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ecifi
c co
nditi
ons.
For a
dditi
onal
info
rmat
ion,
ple
ase
cont
act a
Tec
hnic
al S
ervi
ce R
epre
sent
ativ
e, (8
64) 2
24-3
506
68
S
tyle
W
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Cou
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ount
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F
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W
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Thi
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Stre
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W
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m)
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Fill
22
726
727
728
729
730
731
732
735
736
737
739
740
741
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5 W
RT
Plai
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Plai
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Plai
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Plai
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Plai
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Plai
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Twill
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Plai
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26 26 17 17 22 31 32 35 36 28 39 40 11 22 40 17 17
26 26 17 17 22 31 32 35 36 28 36 40 11 22 40 17 17
Kev
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29 8
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Kev
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29 1
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Kev
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9 15
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Kev
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29 1
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9 40
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0.58
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910
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900
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900
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1800
1950
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3200
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1060
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890
725
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Kevl
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The
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sted
are
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reig
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ntre
ated
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rics.
Act
ual v
alue
s m
ay v
ary.
JPSC
M s
trong
ly re
com
men
ds d
esig
ners
and
use
rs p
erfo
rm
test
ing
for a
pplic
atio
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c co
nditi
ons.
For a
dditi
onal
info
rmat
ion,
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ase
cont
act a
Tec
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al S
ervi
ce R
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sent
ativ
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64) 2
24-3
506
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W
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Cou
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ount
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22
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747
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754
755
756
759
760
768
779
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Bask
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Bask
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Plai
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Plai
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Plai
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17 10 48 29 34 21 21 28 24 30 28 70 20 22 18 22 44
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0.31
0.16
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0.58
0.51
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0.18
0.22
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0.18
0.21
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2000
2000
450
1800
1200
500
350
700
600
720
650
1100
1800
1060
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1300
500
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Kevl
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29,
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The
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sted
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reig
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ntre
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Act
ual v
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ay v
ary.
JPSC
M s
trong
ly re
com
men
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and
use
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rm
test
ing
for a
pplic
atio
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dditi
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info
rmat
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ple
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cont
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Tec
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ervi
ce R
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64) 2
24-3
506
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tyle
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ount
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119
156
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Kevl
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Act
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JPSC
M s
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men
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and
use
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test
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pplic
atio
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info
rmat
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cont
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24-3
506
72
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ount
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0.18
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900
1100
950
1500
500
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700
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600
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1100
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475
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360
550
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Spec
tra ®
Fab
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The
phys
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sted
are
for g
reig
e (u
ntre
ated
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rics.
Act
ual v
alue
s m
ay v
ary.
JPSC
M s
trong
ly re
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men
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ners
and
use
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rm
test
ing
for a
pplic
atio
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ase
cont
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ce R
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64) 2
24-3
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tyle
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ount
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The
phys
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sted
are
for g
reig
e (u
ntre
ated
) fab
rics.
Act
ual v
alue
s m
ay v
ary.
JPSC
M s
trong
ly re
com
men
ds d
esig
ners
and
use
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erfo
rm
test
ing
for a
pplic
atio
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d pa
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nditi
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onal
info
rmat
ion,
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ase
cont
act a
Tec
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al S
ervi
ce R
epre
sent
ativ
e, (8
64) 2
24-3
506
73
Stra
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1346
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302
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Tech
nica
l Ref
eren
ces
- Eng
lish
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.
JPSC
M s
trong
ly re
com
men
ds d
esig
ners
and
use
rs p
erfo
rm
test
ing
for a
pplic
atio
n an
d pa
ckag
e sp
ecifi
c co
nditi
ons.
For a
dditi
onal
info
rmat
ion,
ple
ase
cont
act a
Tec
hnic
al S
ervi
ce R
epre
sent
ativ
e, (8
64) 2
24-3
506
74
75
Stra
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cific
C
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us F
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0.97
1.44
1.44
1.45
2600
4800
2926
2926
3305
3429
3429
3429
2401
2829
3209
3498
3305
3498
72 85 109
75 94 75 94 81 79 103
113
65 90 103
4.0
5.5
2.5
3.3
3.3
3.5
3.4
3.6
3.6
3.1
2.9
3.7
3.3
2.1
13.4
218
.86
20.7
129
.71
23.3
924
.27
24.6
024
.27
25.2
329
.72
33.7
124
.76
23.3
924
.59
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
-2.7
0-2
.20
-2.2
0-2
.20
-2.2
0-2
.20
- - --2
.20
-2.2
0-2
.40
730
850
450
450
450
450
450
450
150
150
150
450
450
450
Tech
nica
l Ref
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- Met
ric
The
phys
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pro
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are
for g
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ay v
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For a
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info
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ple
ase
cont
act a
Tec
hnic
al S
ervi
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epre
sent
ativ
e, (8
64) 2
24-3
506
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+32)*(9/5) 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
76
77
