SIRCA-15F [virgin]

Property: Thermal Conductivity (Isotropic)

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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

Thermal Conductivity (Isotropic)
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Value (Btu/ft-s-R) Pressure (psf) Temperature (R) Uncertainty Uncertainty Source
7.85e-06 2.12 420.0 N/A
7.99e-06 2.12 447.0 N/A
8.06e-06 2.12 474.0 N/A
8.13e-06 2.12 501.0 N/A
8.29e-06 2.12 530.0 N/A
8.70e-06 2.12 855.0 N/A
1.10e-05 2.12 1211.0 N/A
2.04e-05 2.12 1754.0 N/A
1.98e-05 2.12 2273.0 N/A
3.17e-05 2.12 2786.99 N/A
8.06e-06 21.16 420.0 N/A
8.19e-06 21.16 447.0 N/A
8.36e-06 21.16 474.0 N/A
8.47e-06 21.16 501.0 N/A
8.70e-06 21.16 530.0 N/A
9.58e-06 21.16 855.0 N/A
1.16e-05 21.16 1211.0 N/A
2.09e-05 21.16 1754.0 N/A
2.08e-05 21.16 2273.0 N/A
3.24e-05 21.16 2786.99 N/A
8.36e-06 211.62 420.0 N/A
8.63e-06 211.62 447.0 N/A
8.91e-06 211.62 474.0 N/A
9.12e-06 211.62 501.0 N/A
9.47e-06 211.62 530.0 N/A
1.10e-05 211.62 855.0 N/A
1.28e-05 211.62 1211.0 N/A
2.21e-05 211.62 1754.0 N/A
2.40e-05 211.62 2273.0 N/A
3.44e-05 211.62 2786.99 N/A
4.65e-05 211.62 3389.99 N/A