Boltaron 9815M

About
Greater impact resistance than competitive 65/65-rated PVC/Acrylic metallic sheets, plus integral color for unsurpassed scratch resistance Boltaron 9815M is a proprietary, fire retardant, extruded PVC/Acrylic alloy for aircraft interior components that meets stringent FAA requirements for flammability, smoke generation and heat release while exhibiting exceptional physical properties. It offers Izod Impact resistance of 5.0 ft lbs/in. (265 J/m)- higher than competitive 65/65- compliant sheets rated at 3.0 ft lbs/in. (159 J/m)- as well as extreme formability, consistent surface quality, and an unlimited range of colors. And unlike FAR 25.853 (d) rated sheet that is reverse-printed with metallic ink on clear cap film laminated to dissimilar substrate material, Boltaron 9815M is comprised of a cap film with integral metallic coloration, permanently fused to a matching “9815-grade” substrate of a complementary solid color, preventing de-lamination and offering unsurpassed scratch resistance. Since the 9815M monolithic cap film is a “metallized” version of Boltaron’s 9815 solid color substrate, metallic color selection is unlimited. Boltaron 9815M is specified by the world’s leading commercial, military and private aircraft and helicopter manufacturers, carriers and interior refurbishing contractors, for thermoformed, fabricated and machined interior components of unequalled durability and metallic appearance.&&

Product Description
GenericPMMA+PVC
Material StatusCommercial: Active
FeaturesHigh impact resistance,Low smoke,Flame Characteristics,Durability
AvailabilitysNorth America

Technical Data
PHYSICALNominal valueUnitTest method
Density1.57g/cm³ASTM D792
Shrinkage rate
MD0.50 to 0.70%ASTM D955

IMPACTNominal valueUnitTest method
Notched impact strength of cantilever beam
23℃270J/mASTM D256

THERMALNominal valueUnitTest method
Hot deformation temperature
1.8 MPa, annealed76.7ASTM D648
Linear coefficient of thermal expansion
MD3.0E-51/℃ASTM D696

FLAME CHARACTERISTICSNominal valueUnitTest method
exothermic FAR 25.853
2 min< 65kW·min/m²FAR 25.853
Peak< 65kW/m²FAR 25.853

Supplementary informationNominal valueUnitTest method
Ds ASTM F814
1.5 min< 100 ASTM F814
4 min< 200 ASTM F814
Forming temperature168 to 188

MECHANICALNominal valueUnitTest method
Rockwell hardness107 ASTM D785
tensile strength
yield37.9MPaASTM D638
Bending modulus2830MPaASTM D790
bending strength
yield60.0MPaASTM D790

Notes
1. Typical properties: these are not to be construed as specifications.
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