| 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 | |
|---|---|
| Generic | PMMA+PVC |
| Material Status | Commercial: Active |
| Features | High impact resistance,Low smoke,Flame Characteristics,Durability |
| Availabilitys | North America |
| Technical Data | |||
|---|---|---|---|
| PHYSICAL | Nominal value | Unit | Test method |
| Density | 1.57 | g/cm³ | ASTM D792 |
| Shrinkage rate | |||
| MD | 0.50 to 0.70 | % | ASTM D955 |
| IMPACT | Nominal value | Unit | Test method |
|---|---|---|---|
| Notched impact strength of cantilever beam | |||
| 23℃ | 270 | J/m | ASTM D256 |
| THERMAL | Nominal value | Unit | Test method |
|---|---|---|---|
| Hot deformation temperature | |||
| 1.8 MPa, annealed | 76.7 | ℃ | ASTM D648 |
| Linear coefficient of thermal expansion | |||
| MD | 3.0E-5 | 1/℃ | ASTM D696 |
| FLAME CHARACTERISTICS | Nominal value | Unit | Test method |
|---|---|---|---|
| exothermic | FAR 25.853 | ||
| 2 min | < 65 | kW·min/m² | FAR 25.853 |
| Peak | < 65 | kW/m² | FAR 25.853 |
| Supplementary information | Nominal value | Unit | Test method |
|---|---|---|---|
| Ds | ASTM F814 | ||
| 1.5 min | < 100 | ASTM F814 | |
| 4 min | < 200 | ASTM F814 | |
| Forming temperature | 168 to 188 | ℃ |
| MECHANICAL | Nominal value | Unit | Test method |
|---|---|---|---|
| Rockwell hardness | 107 | ASTM D785 | |
| tensile strength | |||
| yield | 37.9 | MPa | ASTM D638 |
| Bending modulus | 2830 | MPa | ASTM D790 |
| bending strength | |||
| yield | 60.0 | MPa | ASTM D790 |
| Notes |
|---|
| 1. Typical properties: these are not to be construed as specifications. |
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