Grants and Contracts Details
Description
The morphology characteristics and ablation behavior of a highly porous carbon ber
preform will be studied. First, the morphological characterization of the three-dimensional
structure of the material will be performed by hard X-rays synchrotron micro-tomography.
The resulting micro-tomography voxels will be used to compute geometrical properties of
the carbon preform, like porosity, specic surface area and tortuosity, that are otherwise
indirectly measured through experimental techniques. The reconstructed volumes are used
to build a computational grid for numerical simulations of the bers' ablation. By modeling
the diusion of oxygen through the porous medium using Lagrangian methods, and the
oxidation at the carbon bers? surface using a reactivity model, the ablation of the carbon
bers will be simulated for a range of Thiele numbers.
Next, the oxidation at high Knudsen number of FiberForm, the matrix material of
NASA's Phenolic Impregnated Carbon Ablator, will also be investigated experimentally
at the NASA Flow Tube facility. The mass loss and recession of carbon preform samples
will be measured at temperatures between 700 and 1300 K and pressures around 2000 Pa.
Using the parametric data obtained by the 3D reconstruction, numerical simulation of that
experiment will be performed and compared to the experimental results.
Status | Finished |
---|---|
Effective start/end date | 7/1/14 → 6/30/15 |
Funding
- National Aeronautics and Space Administration: $64,825.00
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