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)
SI Units (MKS)
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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