STRATOPlate - Space Flight Ready - High Modulus Carbon Fiber
STRATOPlate laminates are space flight ready and are offered as a commercial off-the-shelf (COTS) product for easy purchasing. These plates are an excellent choice for structures that require high stiffness (bending stiffness, first mode frequency, etc.), low CTE, or for pairing with your choice of honeycomb core and film adhesive to make space grade sandwich panels. Full traceability is maintained to material lots, cure cycle detail, and buy-up coupon testing. We offer STRATOPlate configurations designed for both Low Earth Orbit (LEO), and Medium or Geostationary Earth Orbit (GEO) to fit your unique requirements. Can’t find exactly what you’re looking for? Contact us for a custom quote
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Features & Benefits
Each space grade order includes a certificate package with dimensional inspection, material certificates, traceability, and a statement of verification. All plates are serialized and traceable. Additional options include full traveler verification (copies of out-time tracking, ply angle and cure verifications), resin content testing (up to three tests per plate available), and short beam shear testing.
Additional Information
| P/N | 22Z002102-9-0.054-96-48 | 22Z002102-11-0.108-96-48 | 22Z002102-3-0.044-96-48 | 22Z002102-5-0.089-96-48 |
|---|---|---|---|---|
| Application | ||||
| Built To Order | Yes | Yes | Yes | Yes |
| Clearance | ||||
| Color | ||||
| ECCN | ||||
| Finish | Matte / Matte | Matte / Matte | Matte / Matte | Matte / Matte |
| Flexural Strength (ksi) | ||||
| Height | ||||
| HTS - Harmonized Tariff Code | ||||
| Major ID | ||||
| Major OD | ||||
| Materials | High Modulus Carbon | High Modulus Carbon | High Modulus Carbon | High Modulus Carbon |
| Temperature Rating (F) | 300.0 | 300.0 | 450.0 | 450.0 |
| Minor ID | ||||
| Minor OD | ||||
| Plate / Panel Size | ||||
| REACH | ||||
| RoHS | ||||
| Schedule B | ||||
| Space Flight Ready | true | true | true | true |
| Tensile Modulus, msi | 12.6 | 12.6 | 15.8 | 15.8 |
| Tensile Strength (ksi) | 105.2 | 105.2 | 102.9 | 102.9 |
| Thickness | 0.054 | 0.108 | 0.044 | 0.089 |
| Traceability Included | true | true | true | true |
| USMCA Criterion | ||||
| Weight | 13.44 | 26.88 | 12.48 | 25.28 |
| Width | 48.0 | 48.0 | 48.0 | 48.0 |
Technical Data
Technical drawing including layup and cure details is available upon request with NDA.
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Calculated Laminate mechanical properties |
||
| PROPERTY | VALUE | UNITS |
| Ft1u | 105.2 | ksi |
| Fc1u | -73.7 | ksi |
| Ft2u | 105.2 | ksi |
| Fc2u | -73.7 | ksi |
| F12 | 52.6 | ksi |
| E1 | 12.6 | Msi |
| E2 | 12.6 | Msi |
| G12 | 4.91 | Msi |
| v12 | 0.280 | |
| CTE1 | 0.819 | ppm/°F |
| CTE2 | 0.819 | ppm/°F |
As-tested properties are coming soon.
Tolerances
Length: ± 0.125"
Width: ± 0.125"
Thickness: ± 10%
Flatness: 0.050" (0.020/24.0x24.0)