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 …
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 …
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 …
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 …
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 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 …
The spectral and directional dependence of emissivity along with radiative emissions of scattering media has been characterized as functions of the optical thickness, scattering …
Fibrous porous materials are extensively employed as heat shielding material for space vehicles and capsules. To predict the performance of these materials using computational …
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 …