Material Properties DatabaseLI-2200 Rigid Tile
Property: Specific Heat
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Name: LI-2200 Rigid Tile
Database: NASA Ames Thermal Protection Materials
Category: Silicon-Based Reusable Composites: Rigid Ceramic Tiles
Composition: 100% SiO2
Manufacturer: United Space Alliance (USA)
Technical Readiness Level: 9
Last Modified: 2001-10-01
Description:
- LI-2200 is a relatively high density (~22 lbs/cu.ft.) and thermal conductivity fibrous insulation material with higher strength than the LI-900 baselined for use on all the shuttle orbiters. It is currently flying on all orbiters, but to a very limited extent due to itsÕ weight. It was originally developed to provide an enhanced strength RSI tile relative to LI-900.
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 |
|---|---|---|---|---|
| 2.93e+02 | N/A | 116.483 | 84.0 | Measurement limit |
| 4.40e+02 | N/A | 172.039 | 84.0 | Measurement limit |
| 6.28e+02 | N/A | 255.372 | 84.0 | Measurement limit |
| 8.79e+02 | N/A | 394.261 | 87.9 | +/- 10% |
| 1.06e+03 | N/A | 533.15 | 1.06e+02 | +/- 10% |
| 1.15e+03 | N/A | 672.039 | 1.15e+02 | +/- 10% |
| 1.21e+03 | N/A | 810.928 | 1.21e+02 | +/- 10% |
| 1.24e+03 | N/A | 949.817 | 1.24e+02 | +/- 10% |
| 1.26e+03 | N/A | 1088.71 | 1.26e+02 | +/- 10% |
| 1.26e+03 | N/A | 1199.82 | 1.26e+02 | +/- 10% |
| 1.27e+03 | N/A | 1227.59 | 1.27e+02 | +/- 10% |
| 1.27e+03 | N/A | 1366.48 | 1.27e+02 | +/- 10% |
| 1.27e+03 | N/A | 1533.15 | 1.27e+02 | +/- 10% |
| 1.27e+03 | N/A | 1922.04 | 1.27e+02 | +/- 10% |