Flow Mechanics in Ablative Thermal Protection Systems

NN Mansour, F Panerai, J Lachaud… - Annual Review of Fluid …, 2024 - annualreviews.org
Ablative thermal protection systems have experienced renewed interest in the past decade
owing to the retirement of NASA's Space Shuttle fleet and the US presidential mandate to …

Experimental investigation on the validity of the local thermal equilibrium assumption in ablative-material response models

S Liu, A Ahmadi-Senichault, C Levet… - Aerospace Science and …, 2023 - Elsevier
Abstract Thermal Protection Systems (TPS) material response models rely on the
assumption of local thermal equilibrium (LTE) between the solid phase and the gas phase …

Decomposition of carbon/phenolic composites for aerospace heatshields: Detailed speciation of phenolic resin pyrolysis products

F Torres-Herrador, A Eschenbacher, J Coheur… - Aerospace Science and …, 2021 - Elsevier
Abstract Thermal Protection Materials (TPM) such as carbon/phenolic composites are used
to protect spacecraft structures from extreme conditions. This protection is, in part, achieved …

Equilibrium model for the ablation response of silicone-coated PICA

JBE Meurisse, GB Chatzigeorgis, PV Diaz… - International Journal of …, 2023 - Elsevier
A novel equilibrium ablation and thermal response model for NASA's Phenolic Impregnated
Carbon Ablator (PICA) is presented. For the first time, the model accounts for the effect of …

Preliminary experimental study on combustion characteristics in a solid rocket motor nozzle based on the TDLAS system

Y Gao, Y Liu, Z Dong, D Ma, B Yang, C Qiu - Energy, 2023 - Elsevier
A preliminary experimental study on combustion in a nozzle of solid rocket motor is
conducted using a division multiplexing scanning wavelength TDLAS system to accurately …

Assessment of a one-dimensional finite element charring ablation material response model for phenolic-impregnated carbon ablator

Y Wang, TK Risch, JH Koo - Aerospace Science and Technology, 2019 - Elsevier
In this study, mathematical formulations to model charring ablation problems were
numerically implemented using finite element analysis (FEA) with ABAQUS, which account …

A high heating rate pyrolysis model for the Phenolic Impregnated Carbon Ablator (PICA) based on mass spectroscopy experiments

F Torres-Herrador, JBE Meurisse, F Panerai… - Journal of Analytical and …, 2019 - Elsevier
A novel model for the pyrolysis of the Phenolic Impregnated Carbon Ablator (PICA) at high
heating rate is developed and calibrated based on high fidelity thermal decomposition …

Characterization of directional and anisotropic scattering dependency of emissivity for fibrous heat shields under non-isothermal conditions

AH Yassin, SJ Poovathingal - International Journal of Heat and Mass …, 2024 - Elsevier
The spectral and directional dependence of emissivity along with radiative emissions of
scattering media has been characterized as functions of the optical thickness, scattering …

[HTML][HTML] Micro-CT image-based computation of effective thermal and mechanical properties of fibrous porous materials

D Liu, H Chen, LA Chacon, VM Ramu… - Composites Part B …, 2024 - Elsevier
Fibrous porous materials are extensively employed as heat shielding material for space
vehicles and capsules. To predict the performance of these materials using computational …

Aerothermal characterization of the Plasmatron X wind tunnel: heat flux, stagnation pressure and jet unsteadiness

L Capponi, T Oldham, M Konnik, K Stephani… - AIAA Scitech 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1338. vid Inductively coupled
plasma wind tunnels accurately replicate the harsh conditions that hypersonic vehicles …