PLATE - CARBON FIBER - HIGH TEMP (402F Tg) BALANCED - PEEL PLY / PEEL PLY - 24 X 48 X 0.25 INCH (*Note length & width tolerance of +/-0.375" due to blade kerf)
0.25" x 24" x 48"
1
-
10
$804.99
11
-
49
$679.79
50
+
$620.59
The Available Quantity listed above is what we have in inventory for this item. Provided there has not been a prior sale, you can expect an order placed today, for this quantity or less, to ship the next business day. For quantities over the number available:
Generally available to ship in two to four weeks.
PLATE - CARBON FIBER - HIGH TEMP (402F Tg) BALANCED - PEEL PLY / PEEL PLY - 24 X 48 X 0.25 INCH
Press cured, balanced carbon fiber & epoxy resin prepreg laminates. These laminate plates (panels) are made with a nylon peel ply co-cured on both outer surfaces of the laminate which may be removed by the user. This plate was originally designed for use in tooling applications as backing structures although its use expands far beyond.
Additional Information
| P/N | PLATE-HT025-24 |
|---|---|
| Finish | Matte / Matte |
| HTS - Harmonized Tariff Code | 6815.13.0000 |
| Materials | High Temperature Carbon |
| Plate / Panel Size | 24" x 48" / 609.6mm x 1219.2mm |
| Thickness | 0.25 |
| Weight | 17.29 |
| Width | 24.0 |
Technical Data
Standard Modulus carbon fiber and epoxy laminate with a 0/90 orientation throughout. and a plain weave on the outside.
- Glass Transition Temp (Tg): 402 F
- Coefficient of thermal expansion, X-Y: 2.34 to 2.91
Structural Properties
- @ Room Temperature
- Flexural Strength: 121.9 ksi
- Flexural Modulus: 8.9 Msi
- @ 350 F
- Flexural Strength: 49.8 ksi
- Flexural Modulus: 7.4 Msi
Structural Properties after 100 cycles
- @ Room Temperature
- Flexural Strength: 122.8 ksi
- Flexural Modulus: 9.1 Msi
- @ 350 F
- Flexural Strength: 58.7 ksi
- Flexural Modulus: 8.1 Msi
*No warranty of fitness for a particular purpose are made. Values supplied here should be validated by testing in your specific application.