0.750" x 0.832" x 72" ◾ Space Grade LEO
Rock West Composites is proud to introduce a line of tubes specifically crafted for the rigors of space. Constructed with HR40 carbon fiber (57 Msi) in a quasi-isotropic layup for low CTE and high stiffness. NB321 resin is used to ensure low outgassing and reliable performance for multiple years on station. Designed specifically for Low Earth Orbit (LEO), the maximum suggested use temperature is 300°F (150°C). Full traceability is maintained to material lots, cure cycle detail, and buy-up coupon testing.
Each space grade order includes a certificate package with dimensional inspection, material certificates, traceability, and a statement of verification. All tubes 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 two test per tube available), and short beam shear testing.
Mitsubishi HR40 high modulus fiber.
Newport 321 epoxy resin.
Application | Space & Stable Structures |
---|---|
Shape | Round |
Materials | High Modulus Carbon |
Pattern | Unidirectional |
Color | Black |
Finish | Cello Wrap Gloss |
Inside Diameter | 0.75 |
Outside Diameter | 0.832 |
Wall Thickness | 0.041 |
Length | 72 |
Length (max continuous) | 72.0 |
Linear Density | 0.07 |
Volumetric Density | 0.057 |
Weight | 0.418 |
Primary Fiber | Tenax UTS50 |
Primary Resin / Hardener | Eporite EHM32 |
Resin / Chemistry / Polymer Type | Epoxy |
Space Flight Ready | true |
All laminate properties and mechanical calculations are based on Classical Lamination Theory and should be used as a reference only. Rock West Composites does not guarantee these properties or calculations.
Avg EX Young's Modulus | 1.257E7 |
---|---|
Avg EY Young's Modulus | 1.257E7 |
GXY Shear Modulus | 4909000.0 |
X Tensile Yield Strength | 86450.0 |
X Compressive Yield Strength | 73650.0 |
Y Tensile Yield Strength | 82780.0 |
Y Compressive Yield Strength | 80770.0 |
XY Shear Strength | 41640.0 |
CTEX | 8.19E-07 |
CTEY | 8.19E-07 |
Poisson's Ratio vXY | 0.28 |
Poisson's Ratio vYX | 0.28 |
All laminate properties and mechanical calculations are based on Classical Lamination Theory and should be used as a reference only. Rock West Composites does not guarantee these properties or calculations.
Ply # | Orientation (degrees) | Location |
---|---|---|
1 | 0 | Inside |
2 | 60 | ↓ |
3 | -60 | |
4 | -60 | |
5 | 60 | |
6 | 0 | |
7 | 0 | |
8 | 60 | |
9 | -60 | |
10 | -60 | |
11 | 60 | |
12 | 0 | Outside |
Calculated tube laminate mechanical properties |
||
PROPERTY | VALUE | UNITS |
Ft1u | 121.5 | ksi |
Fc1u | -73.7 | ksi |
Ft2u | 107.6 | ksi |
Fc2u | -108 | ksi |
F12 | 52.6 | ksi |
E1 | 12.57 | Msi |
E2 | 12.57 | Msi |
G12 | 4.91 | Msi |
v12 | 0.280 | |
CTE1 | 0.819 | ppm/°F |
CTE2 | 0.819 | ppm/°F |
As-tested properties are coming soon.
ID: ± 0.003"
Wall: ± 10%
Length: ± 0.125"
Straightness: 0.006"/ft TIR
We use cookies to improve the operation of our websites. By using our websites you agree that we may store cookies on your device. You can learn more about how we use cookies by reviewing our Privacy Policy.