SIRCA-15F [virgin]
Property: Specific Heat
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Name: SIRCA-15F [virgin]
Database: NASA Ames Thermal Protection Materials
Category: Silicon-Based Ablators
Composition: FRCI-12 tile, infiltrated w/ silicone
Manufacturer: NASA Ames Research Center, Thermal Protection Materials and Systems Branch
Technical Readiness Level: 9
Last Modified: 2001-10-01
Description:
- SIRCA-15F uses the Fibrous Refractory Ceramic Insulation, with 0.192 g/cc density (FRCI-12) tile substrate and is impregnated with silicone to produce a material with a final density of approximately 0.25 g/cc. SIRCA-15F was used for the aft plate heat shield and a portion of the conical aft section of the Mars/Pathfinder probe, which successfully landed on the Martian surface in July 1997. SIRCA-15F was designed, tested, and manufactured for the X-34 Program as a re-usable TPS for the nosecap and wing and rudder leading edges. SIRCA-15F is also being manufactured to support the Backshell Interface Plate (BIP) for the Mars 2003 Mission.
Point of Contact:
- Frank S. Milos
- NASA Ames Research Center
- fmilos@mail.arc.nasa.gov
Specific Heat
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| Value (J/kg-K) | Pressure (Pa) | Temperature (K) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 1.09e+03 | N/A | 233.333 | N/A | |
| 1.10e+03 | N/A | 236.667 | N/A | |
| 1.10e+03 | N/A | 245.556 | N/A | |
| 1.11e+03 | N/A | 251.667 | N/A | |
| 1.11e+03 | N/A | 257.778 | N/A | |
| 1.11e+03 | N/A | 267.778 | N/A | |
| 1.12e+03 | N/A | 276.667 | N/A | |
| 1.12e+03 | N/A | 292.222 | N/A | |
| 1.13e+03 | N/A | 307.222 | N/A | |
| 1.15e+03 | N/A | 475.0 | N/A | |
| 1.16e+03 | N/A | 672.778 | N/A | |
| 1.20e+03 | N/A | 974.445 | N/A | |
| 1.24e+03 | N/A | 1262.78 | N/A | |
| 1.27e+03 | N/A | 1548.33 | N/A |
Material Properties Database