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
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| Value (Btu/lbm-R) | Pressure (psf) | Temperature (R) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 7.00e-02 | N/A | 209.67 | 2.01e-02 | Measurement limit |
| 1.05e-01 | N/A | 309.67 | 2.01e-02 | Measurement limit |
| 1.50e-01 | N/A | 459.67 | 2.01e-02 | Measurement limit |
| 2.10e-01 | N/A | 709.67 | 2.10e-02 | +/- 10% |
| 2.52e-01 | N/A | 959.67 | 2.53e-02 | +/- 10% |
| 2.75e-01 | N/A | 1209.67 | 2.75e-02 | +/- 10% |
| 2.88e-01 | N/A | 1459.67 | 2.89e-02 | +/- 10% |
| 2.96e-01 | N/A | 1709.67 | 2.96e-02 | +/- 10% |
| 3.00e-01 | N/A | 1959.68 | 3.01e-02 | +/- 10% |
| 3.02e-01 | N/A | 2159.68 | 3.01e-02 | +/- 10% |
| 3.03e-01 | N/A | 2209.66 | 3.03e-02 | +/- 10% |
| 3.03e-01 | N/A | 2459.66 | 3.03e-02 | +/- 10% |
| 3.03e-01 | N/A | 2759.67 | 3.03e-02 | +/- 10% |
| 3.03e-01 | N/A | 3459.67 | 3.03e-02 | +/- 10% |