SLA-561V [virgin]
Property: Specific Heat
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Name: SLA-561V [virgin]
Database: NASA Ames Thermal Protection Materials
Category: Silicon-Based Ablators
Composition: N/A
Manufacturer: N/A
Technical Readiness Level: N/A
Last Modified: 1996-08-01
Description:
- Silicone based ablator incorporating a reinforcing honeycomb manufactured by Lockheed Martin and used as the primary heatshield for the Mars Viking Missions. Sla-561V consists of a mixture of silicone, silica microballoons, corks and silica glass fibers. This mixture is then injected into the phenolic honeycomb cells. <BR><BR> SLA-561V was also baselined as the forebody heatshield the Mars/Pathfinder probe which is scheduled to be launched in December 1996 and arriving at the martian surface in July 1997. The main difference between the SLA-561V fore Viking and Mars/Pathfinder is the size of the honeycomb cells and the heat shield thickness. The Mars/Pathfinder uses a smaller honeycomb cells and has a thickness of 0.75 in. The increase in thickness is necessary because the peak heating rate on Mars/Pathfinder is predicted to be around 120 Btu/sqft-s with stagnation pressure of 0.25 atm.
Point of Contact:
- Frank S. Milos
- NASA Ames Research Center
- fmilos@mail.arc.nasa.gov
Specific Heat
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| Value (Btu/lbm-R) | Pressure (psf) | Temperature (R) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 2.05e-01 | N/A | 1.0 | N/A | |
| 2.05e-01 | N/A | 250.0 | N/A | |
| 2.05e-01 | N/A | 310.0 | N/A | |
| 2.62e-01 | N/A | 460.0 | N/A | |
| 2.72e-01 | N/A | 500.0 | N/A | |
| 2.77e-01 | N/A | 510.0 | N/A | |
| 2.85e-01 | N/A | 560.0 | N/A | |
| 2.88e-01 | N/A | 750.0 | N/A | |
| 2.90e-01 | N/A | 760.0 | N/A | |
| 2.90e-01 | N/A | 800.0 | N/A | |
| 2.90e-01 | N/A | 1000.0 | N/A | |
| 2.90e-01 | N/A | 1160.0 | N/A |
Material Properties Database