ARTIFICAL REINFORCEMENTSYNTHETIC COMPOSITE MATERIAL PROPERTIES MATERIALS MODE OF EXISTS
vinay: prepregs are all inculded in sheet2DENSITY(g/cm3)VOLUME(cm3)
vinay: weight is calculated for 1m*1m*1mmMASS (kg) TENSILE STRENGTH (Mpa)TENSILE MODULUS (Gpa)SHEAR STRENGTH COST ($/lb)STIFFNESS(N/m)
vinay: vinay:considering acceleration due to gravity(9.81) involved within the existing mass(matter) APPLICATIONAluminafiber3.310003.3600210-220 --05-200Aluminium sheet 2.710002.750072--0.75steel sheet 7.8510007.851500207--0.1carbon fiberPAN 1.75-1.9010001.752413.1-6894200--20-100PITCH1.90-2.1510001.91378-3102189--40-200RAYON1.610001.6103442--05-25Glass fiberE-GLASS2.5910002.59344572.35--05-40S-GLASS2.4610002.46461986.81--05-40H22.4910002.49461986.81--05-40Armidefiber1.4410001.443400173--25-75BORONfiber2.3-2.610002.35033389--100-250

NATURAL REINFORCEMENTCOMPOSITE NATURAL MATERIAL PROPERTIES MATERIALS MODE OF EXISTS
vinay: prepregs are all inculded in sheet2DENSITY(g/cm3)VOLUME(cm3)
vinay: weight is calculated for 1m*1m*1mmMass (kg) TENSILE STRENGTH (Mpa)TENSILE MODULUS (Gpa)STIFFNESS(N/m)
vinay: vinay:considering acceleration due to gravity(9.81) involved within the existing mass(matter) cost ($/lb)ApplicationCOTTONFIBRE1.610001.62875.5FLAXFIBRE1.510001.534527.6HEMPFIBRE1.510001.569070SISALFIBRE1.510001.55119.4RAMIEFIBRE1.510001.540061.4KENAFFIBRE1.410001.493053JUTEFIBRE1.310001.339326.5COIRFIBRE1.210001.21754BAMBOOFIBRE1.3210001.32400

PREPREG_SELECTION_GUIDEPREPREG SELECTION

HEXPLY PREPREGREINFORCEMENT MATRIX LAMINATE DENSITY STRENGTH(Mpa)SHELF LIFE CURING GSM (g/m)THICKNESS (mm)APPLICATIONTENSILE COMPRESSIVE TemperatureTIME

M47_euCARBON - UD, WOVEN EPOXY---1823-9201015-715MAX at -18C (0F).1400C90min 193---BODY OF AUTOMOBILE, SMOOTH AND TRANSPERANCY,AUTOCLAVEM49_euCARBON EPOXY---104060012 months at -18C (0F)1200C60min 3700.4BODY OF AUTOMOBILE HexPlyM9M10GLASS- UD & FABRICEPOXY---130090012 months at -18C (0F)1200C60min 12000.666BODY OF AUTOMOBILE,VACCUM ONLY, LEAF SPRING, FISH PLATES(RAILS)CARBON- UD & FABRICSEPOXY---90560012 months at -18C (0F)1200C60min 600BODY OF AUTOMOBILE,VACCUM ONLY, LEAF SPRING, FISH PLATES(RAILS)M91F_M96F_eu---EPOXY ---------12 months at -18C (0F)1200C30min ------BODY OF AUTOMOBILE, WIND ENERGY,FISH PLATES(RAILS), SMOOTH & TRANSPERANCY,VACCUM ONLY M35_4_euCARBON EPOXY1.5483088012 months at -18C (0F)1500C30min 3850.398CHASSIS, SMOOTH & TRANSPERANCY,AUTOCLAVEM48_euCARBON EPOXY1.572895169312 months at -18C (0F)1800C120min 1500.147CHASSISM21_globalCARBON EPOXY1.583050150012 months at -18C (0F)---------0.184OTHER AUTOMOBILE M34_euGLASSEPOXY---60054012 months at -18C (0F)1200C40min 300---MARINE,RAILS(LARGE STRUCTURES), VACCUM ONLYCARBONEPOXY---90060012 months at -18C (0F)1200C40min 600---EF01euGLASSEPOXY---450---14 months at -18C (0F)120 C15 min300---TRANSPERENT AND SMOOTHING, VACCUM ONLY CARBONEPOXY---2000120014 months at -18C (0F)120 C15 min300---TRANSPERENT AND SMOOTHING, VACCUM ONLY HexPly SCARBON, GLASS EPOXY ---------6 months at -18C (0F)100 C15 min------short curing cycles for sporting (e.g. in ski production)M77PREPREGGLASSEPOXY---480---18 months at -18C (0F)150 C2 min106--- ski production,SPORTSCARBONEPOXY---2400---18 months at -18C (0F)150 C2 min600--- ski production,SPORTSHexPly_M52_euCARBON-UDEPOXY1.51500---18 months at -18C (0F)120 C15 min1500.161AUTOCLAVE,PCMCARBON- FABRICSEPOXY1.4975160418 months at -18C (0F)120 C15 min1930.216AUTOCLAVE,PCMEH04GLASSEPOXY---------18 months at -18C (0F)121 C15 min193---SHRINK WARP, VACCUM, PCMCARBONEPOXY---2230153018 months at -18C (0F)121 C15 min120---SHRINK WARP, VACCUM, PCMM81PREPREGCARBONEPOXY1.55110084012 months at -18C (0F)1350C180 min3700.41CHASSIS, AUTOCLAVE

MATRICES PROPERTIESTHERMOSET MATRICES(RESINS or MATRICES)SL.no MaterialsDensity(g/cm3)Modulus(Mpa)Tensile strength(Mpa)Elongation to failure(%)Thermal conductivity CTE(10-6 m/(m 0c))1EPOXIES1.1-1.43000-600035-100(1-6)0.1602POLYESTERS1.2-1.52000-450040-9020.2100-2003VINYLESTERS 1-1.2115801014.50.21(-)30 -1004PHENOLICS1.41-1.84---34-41---0.460-805BMI1.51830070.60.9---286cynate1.243000692.59---28.2

SELECTION OF MATRICESSELECTION OF MATRICESMATRICESApplications Limitations EPOXY Structural applicationCannot be used with chopped strand mat High-strength projects Adhesion to metal. Not UV stable. Will deteriorate without a top coat when exposed to UV rays. VINYL ESTERS Gas tanks3 month shelf-life Boat hullsHeat resistant applications. POLYESTERS Corrosion resistant applications.Cannot be used for high strength applications Mold applications PHENOLIC Automotive Applications - Friction Materials for Brake Pad or Disc,Low adhesive propertyAerospace applications-HIGH TEMP PARTS/ENGINES BISMALEIMIDE Aerospace applications-HIGH TEMP PARTS/ENGINES High cost CYANATE Electrical AppliancesExcellent moisture resistance