SIRCA-15F [virgin]
Property: Effective Heat of Ablation
<< Return to Material Data
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
Effective Heat of Ablation
Eng
Switch to SI Units (MKS)
Export Data (Coming Soon!)
| Value (Btu/lbm) | Pressure (psf) | Temperature (R) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 4.76e+05 | 211.62 | N/A | N/A | |
| 2.43e+06 | 317.43 | N/A | N/A | |
| 2.40e+06 | 317.43 | N/A | N/A | |
| 1.41e+05 | 423.24 | N/A | N/A | |
| 3.43e+04 | 634.87 | N/A | N/A | |
| 1.73e+04 | 846.49 | N/A | N/A |
Material Properties Database