One-Dimensional Thermal Analysis Model for Charring Ablative Materials
This paper presents a one-dimensional model for the analysis of the charring ablative materials used in spacecraft thermal protection systems. The numerical method is based on an implicit finite difference formulation of the governing equations written for a system of mobile coordinates that accoun...
Main Author: | Antonio Mazzaracchio |
---|---|
Format: | Article |
Language: | English |
Published: |
Instituto de Aeronáutica e Espaço (IAE)
2018-02-01
|
Series: | Journal of Aerospace Technology and Management |
Subjects: | |
Online Access: | https://www.jatm.com.br/jatm/article/view/965 |
Similar Items
-
Comprehensive Comparison of Different Integrated Thermal Protection Systems with Ablative Materials for Load-Bearing Components of Reusable Launch Vehicles
by: Stefano Piacquadio, et al.
Published: (2023-03-01) -
Development and preclinical evaluation of multifunctional hydrogel for precise thermal protection during thermal ablation
by: Bowen Zheng, et al.
Published: (2024-01-01) -
Computational modeling of microwave ablation with thermal accelerants
by: Jan Sebek, et al.
Published: (2023-12-01) -
Loosely coupled analysis strategy for melt-ablation modeling of thermal protection material in supersonic gas-particle two-phase impingement flow
by: Chong-You Lai, et al.
Published: (2023-10-01) -
Delamination Detection in Polymeric Ablative Materials Using Pulse-Compression Thermography and Air-Coupled Ultrasound
by: Stefano Laureti, et al.
Published: (2019-05-01)