SLA-561V [virgin]
Property: Thermal Conductivity (Isotropic)
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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
Thermal Conductivity (Isotropic)
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| Value (W/m-K) | Pressure (Pa) | Temperature (K) | Uncertainty | Uncertainty Source |
|---|---|---|---|---|
| 3.74e-02 | N/A | 0.555556 | N/A | |
| 3.74e-02 | N/A | 138.889 | N/A | |
| 4.24e-02 | N/A | 172.222 | N/A | |
| 5.73e-02 | N/A | 255.556 | N/A | |
| 5.79e-02 | N/A | 277.778 | N/A | |
| 5.92e-02 | N/A | 283.333 | N/A | |
| 6.73e-02 | N/A | 311.111 | N/A | |
| 8.60e-02 | N/A | 416.667 | N/A | |
| 8.85e-02 | N/A | 422.222 | N/A | |
| 9.35e-02 | N/A | 444.444 | N/A | |
| 9.35e-02 | N/A | 555.556 | N/A | |
| 9.35e-02 | N/A | 644.445 | N/A |
Material Properties Database