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| Material | Carbon/Epoxy Laminate |
| Max Tg (DMA) | 400ºF (191ºC) |
| Flexural Strength/Modulus Strength @ RT | 121.9 ksi (8.9 msi) |
| Flexural Strength/Modulus Strength @ 350ºF | 49.8 ksi (7.4 msi) |
| Flex Str./Mod Str. @ RT after 100 thermal cycles | 122.8 ksi (9.1 msi) |
| Flex Str./Mod Str. @ 350ºF after 100 thermal cycles | 58.7 ksi ( 8.1 msi) |
| CTE, X-Y (by TMA, um/mdegºC) | 2.34 to 2.91 |
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