1/4" Rohacell 31 foam/carbon cloth Aircraft Skin Composite - 0.2953" thick - Composite Structures Technology

Property: Thermal Conductivity (Thru-the-Thickness)

<< Return to Material Data

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 (Thru-the-Thickness)
Eng
Switch to SI Units (MKS)
Export Data (Coming Soon!)

Value (Btu/ft-s-R) Pressure (psf) Temperature (R) Uncertainty Uncertainty Source
1.72e-05 N/A 527.69 8.59e-08 Significant digits reported
1.75e-05 N/A 545.69 8.75e-08 Significant digits reported
1.78e-05 N/A 563.69 8.91e-08 Significant digits reported
1.81e-05 N/A 581.69 9.07e-08 Significant digits reported
1.81e-05 N/A 599.69 9.07e-08 Significant digits reported
1.85e-05 N/A 617.69 9.23e-08 Significant digits reported
1.89e-05 N/A 635.69 9.47e-08 Significant digits reported
1.94e-05 N/A 653.69 9.71e-08 Significant digits reported