In the early days of space exploration, the development of thermal protection systems for reentry vehicles was mainly based on an experimental approach, both for design of …
H Weng, A Martin - Journal of Thermophysics and Heat Transfer, 2014 - arc.aiaa.org
The behavior of pyrolysis gas transport in arcjet test samples is numerically studied. The simulation of the pyrolysis gas flow inside a porous material is presented, using two different …
A Martin, ID Boyd - Journal of Spacecraft and Rockets, 2015 - arc.aiaa.org
The steps necessary to achieve the strong coupling between a flowfield solver and a material response solver are presented. This type of coupling is required to accurately …
Ablation of certain highly volatile materials, such as camphor, naphthalene, and dry ice, can be achieved at relatively mild hypersonic conditions in unheated wind tunnels. This provides …
Thermomechanical analysis of ablative materials is of great importance to the design of thermal-protection systems. A finite volume method for coupling the mechanical and thermal …
A series of experiments was performed to obtain permeability data on FiberForm®, a commercial carbon preform used for manufacturing thermal protection systems. A porous …
H Weng, A Martin - Journal of Thermophysics and Heat Transfer, 2015 - arc.aiaa.org
An orthotropic material model is implemented in a three-dimensional material response code, and numerically studied for charring ablative material. Model comparison is performed …
The multidimensional geometric effects within the heat shield of the Stardust sample return capsule are studied over its reentry trajectory, using a material response solver. The solver …
The geometric effects of iso-Q sample–a geometry that is widely used in arc-jet experiments– were numerically studied on charring ablative materials under arc-jet conditions. The …