STRATOPlate - Space Flight Ready - High Modulus Carbon Fiber

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Space Grade LEO ◾ High Modulus ◾ 48" x 96" x 0.054"
P/N: 22Z002102-9-0.054-96-48
$11,054.00
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Laminate - Space Grade - HR40 - Epoxy - Quasi-iso Unidirectional - 96.0 x 48.0 x 0.054 inch
P/N 22Z002102-9-0.054-96-48
Space Grade LEO ◾ High Modulus ◾ 48" x 96" x 0.108"
P/N: 22Z002102-11-0.108-96-48
$16,674.00
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Laminate - Space Grade - HR40 - Epoxy - Quasi-iso Unidirectional - 96.0 x 48.0 x 0.108 inch
P/N 22Z002102-11-0.108-96-48
Space Grade GEO ◾ High Modulus ◾ 48" x 96" x 0.044"
P/N: 22Z002102-3-0.044-96-48
$27,431.00
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Laminate - Space Grade - M55J - Cyanate Ester - Quasi-iso Unidirectional - 96.0 x 48.0 x 0.044 inch
P/N 22Z002102-3-0.044-96-48
Space Grade GEO ◾ High Modulus ◾ 48" x 96" x 0.089"
P/N: 22Z002102-5-0.089-96-48
$49,277.00
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Laminate - Space Grade - M55J - Cyanate Ester - Quasi-iso Unidirectional - 96.0 x 48.0 x 0.089 inch
P/N 22Z002102-5-0.089-96-48
Estimated lead time for quantities greater than what is Available Now is expected to be between 2 and 4 weeks.

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
Materials High Modulus Carbon High Modulus Carbon High Modulus Carbon High Modulus Carbon
Pattern Unidirectional Unidirectional Unidirectional Unidirectional
Color Black Black Black Black
Finish Matte / Matte Matte / Matte Matte / Matte Matte / Matte
Panel Thickness 0.054400 0.108800 0.044800 0.089600
Width 48.0 48.0 48.0 48.0
Thickness 0.054 0.108 0.044 0.089
Length 96 96 96 96
Weight 13.44 26.88 12.48 25.28
Temperature Rating (F) 300.0 300.0 450.0 450.0
Max Operating Temp- (Tg) 300F to 349F 300F to 349F 350F+ 350F+
Resin / Chemistry / Polymer Type Epoxy Epoxy Cyanate Ester Cyanate Ester
Space Flight Ready true true true true

Technical Specifications

Technical drawing including layup and cure details is available upon request with NDA.

 

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)

Contact Info
STRATOPlate - Space Flight Ready - High Modulus Carbon Fiber
P/N STRATO-PLATE