1/4" Rohacell 31 foam/carbon cloth Aircraft Skin Composite - 0.2953" thick - Composite Structures Technology
Property: Thermal Conductivity (In-Plane)
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Name: 1/4" Rohacell 31 foam/carbon cloth Aircraft Skin Composite - 0.2953" thick - Composite Structures Technology
Database: NASA Langley Research Center Database
Category: Structural Organic Composites
Composition: N/A
Manufacturer: N/A
Technical Readiness Level: 4
Last Modified: 2003-07-30
Description:
- Dimensions: 1ft x 1/4 ft x 1/4 in or 0.3048 m x 0.0762 m x 0.00635 m Composite layer breakdown: pre-pregged carbon cloth, 1/4" (0.00635 m) thick Rohacell 31 foam (2 lb/ft^3), pre-pregged carbon cloth Total specimen: 0.0075 m thick, diameter is 0.048022 cm, 0.00391712 kg Proposed aircraft skin for the blended wing aircraft.
Point of Contact:
- Stephan Adam Ryan
- NASA Langley Research Center
- R.A.STEPHAN@LaRC.NASA.GOV
Thermal Conductivity (In-Plane)
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| Value (Btu/ft-s-R) | Pressure (psf) | Temperature (R) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 3.19e-05 | N/A | 533.09 | 3.21e-07 | measurement uncertainty |
| 3.58e-05 | N/A | 610.49 | 8.02e-07 | measurement uncertainty |
| 3.98e-05 | N/A | 659.09 | N/A |
Material Properties Database