Thermal–Structural Coupled Analysis and Design of a Reentry Capsule with Ablative Thermal Protection Systems

This publication has 24 references indexed in Scilit:

• Heat transfer and pyrolysis gas flow characteristics of light-weight ablative thermal protection system in the blunt body
  International Journal of Thermal Sciences, 2022
• Design and efficiency assessment of hybrid thermal protection structures for return capsule reentry
  Case Studies in Thermal Engineering, 2022
• Thermal response and surface recession of a carbon-phenolic charring heatshield of spacecraft: Numerical simulation and validation
  Journal of Space Safety Engineering, 2022
• Advanced sandwich structures for thermal protection systems in hypersonic vehicles: A review
  Composites Part B: Engineering, 2021
• Thermal protection systems for space vehicles: A review on technology development, current challenges and future prospects
  Acta Astronautica, 2020
• Assessment of a one-dimensional finite element charring ablation material response model for phenolic-impregnated carbon ablator
  Aerospace Science and Technology, 2019
• Optimum design of ablative thermal protection systems for atmospheric entry vehicles
  Applied Thermal Engineering, 2017
• Recent advances in the aerothermodynamics of spiked hypersonic vehicles
  Progress in Aerospace Sciences, 2011
• Thermo-structural behaviour of an UHTC made nose cap of a reentry vehicle
  Acta Astronautica, 2009
• Numerical Simulation of control of plasma flow with magnetic field for thermal protection in Earth reentry flight
  IEEE Transactions on Plasma Science, 2006