1/4" Rohacell 31 foam/carbon cloth Aircraft Skin Composite - 0.2953" thick - Composite Structures Technology
Property: Specific Heat
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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
Specific Heat
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| Value (J/kg-K) | Pressure (Pa) | Temperature (K) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 9.67e+02 | N/A | 296.16 | 4.84 | Significant digits reported |
| 1.02e+03 | N/A | 303.16 | 5.1 | Significant digits reported |
| 1.05e+03 | N/A | 308.16 | 5.25 | Significant digits reported |
| 1.09e+03 | N/A | 313.16 | 5.45 | Significant digits reported |
| 1.12e+03 | N/A | 318.16 | 5.6 | Significant digits reported |
| 1.15e+03 | N/A | 323.16 | 5.75 | Significant digits reported |
| 1.18e+03 | N/A | 328.16 | 5.9 | Significant digits reported |
| 1.20e+03 | N/A | 333.16 | 6.0 | Significant digits reported |
| 1.23e+03 | N/A | 338.16 | 6.15 | Significant digits reported |
| 1.25e+03 | N/A | 343.16 | 6.25 | Significant digits reported |
| 1.27e+03 | N/A | 348.16 | 6.35 | Significant digits reported |
| 1.29e+03 | N/A | 353.16 | 6.45 | Significant digits reported |
| 1.32e+03 | N/A | 358.16 | 6.6 | Significant digits reported |
| 1.33e+03 | N/A | 363.16 | 6.65 | Significant digits reported |
| 1.35e+03 | N/A | 366.16 | 6.75 | Significant digits reported |
Material Properties Database