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 (Btu/ft-s-R) Pressure (psf) Temperature (R) Uncertainty Uncertainty Source
6.00e-06 N/A 1.0 N/A
6.00e-06 N/A 250.0 N/A
6.80e-06 N/A 310.0 N/A
9.20e-06 N/A 460.0 N/A
9.30e-06 N/A 500.0 N/A
9.50e-06 N/A 510.0 N/A
1.08e-05 N/A 560.0 N/A
1.38e-05 N/A 750.0 N/A
1.42e-05 N/A 760.0 N/A
1.50e-05 N/A 800.0 N/A
1.50e-05 N/A 1000.0 N/A
1.50e-05 N/A 1160.0 N/A