Material Properties DatabaseTUFI Composite Surface
Property: Specific Heat
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Name: TUFI Composite Surface
Database: NASA Ames Thermal Protection Materials
Category: Silicon-Based Reusable Composites: Rigid Ceramic Tiles
Composition: 2.5% SiB4, 77.5% (5.75% B2O3, 94.25% SiO2), 20% MoSi2
Manufacturer: Boeing, United Space Alliance (USA)
Technical Readiness Level: 8
Last Modified: 2001-10-01
Description:
- TUFI, or Toughened Uni-piece Fibrous Insulation, is a functional gradient material possessing high emissivity, high temperature capability, toughness, and whose properties can be tailored, or adjusted to specific requirements.
Point of Contact:
- Daniel Leiser
- NASA Ames Research Center
- dleiser@mail.arc.nasa.gov
Specific Heat
SI Units (MKS)
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| Value (J/kg-K) | Pressure (Pa) | Temperature (K) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 7.95e+02 | N/A | 255.556 | 39.8 | Significant digits reported |
| 9.00e+02 | N/A | 394.444 | 45.0 | Significant digits reported |
| 1.00e+03 | N/A | 533.333 | 50.2 | Significant digits reported |
| 1.09e+03 | N/A | 672.222 | 54.4 | Significant digits reported |
| 1.19e+03 | N/A | 811.111 | 59.7 | Significant digits reported |
| 1.26e+03 | N/A | 950.0 | 62.8 | Significant digits reported |
| 1.32e+03 | N/A | 1088.89 | 65.9 | Significant digits reported |
| 1.38e+03 | N/A | 1227.78 | 69.1 | Significant digits reported |
| 1.44e+03 | N/A | 1366.67 | 72.2 | Significant digits reported |
| 1.50e+03 | N/A | 1505.56 | 74.9 | Significant digits reported |
| 1.54e+03 | N/A | 1644.44 | 77.2 | Significant digits reported |
| 1.60e+03 | N/A | 1783.33 | 79.8 | Significant digits reported |