What is it about?
A radiative transfer code is coupled to a thermal response solver to model the internal energy propagation inside the heat shield of spacecraft. The results show that for certain conditions, the temperature distribution can be significantly different.
Featured Image
Read the Original
This page is a summary of: Radiative Transmission and Absorption Within the Thermal Protection System of Atmospheric Entry Spacecraft, Journal of Spacecraft and Rockets, September 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35029.
You can read the full text:
Contributors
The following have contributed to this page
