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Description
Spallation Particle Characterization for Ablative Thermal Protection Systems
Abstract
Spallation is a phenomenon in which solid particles are ejected off the surface of an ablative
material in a high-enthalpy, high-shear flow field. The main contributor to this phenomenon in
carbon-based heat shields is the mechanical erosion of carbon fibers weakened by oxidation
decomposition. The dynamics of this phenomenon, which are poorly characterized in the
literature, strongly affect the ablation rate of the material. In state-of-the-art codes, ablation by
spallation is modeled using a "failure" ablation rate that is empirically determined.
The present study aims at experimentally investigating spallation products ejected in the flow
field and using this information to estimate the importance of spallation in the rate of ablation of
low-density carbon/phenolic materials. Results will be obtained from a test campaign to be
performed at the NASA Langley HYMETS arc jet facility, including direct particle capture and
high-speed multi-camera imagery, will be used to measure the dimensions and characteristics of
particles emitted from carbon-fiber samples exposed to an arc jet airflow. The purpose of this
graduate fellowship request is to support Ms. Kristen Price''s graduate research developing and
conducting the experiment, as well as analyzing its results.
Status | Finished |
---|---|
Effective start/end date | 8/1/20 → 7/31/21 |
Funding
- National Aeronautics and Space Administration
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Projects
- 1 Active
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NASA Kentucky Space Grant Consortium Program 2020-2024
Martin, A. (PI), Renfro, M. (CoI) & Smith, S. (CoI)
National Aeronautics and Space Administration
2/4/20 → 2/3/25
Project: Research project