Thermal Engineering of Mars Entry Carbon/Carbon Non-Ablative Aeroshell - Part 2
Candidate Aeroshell Test models composed of a quasi-isotropic Carbon/Carbon (C/C) front face sheet (F/S), eggcrate core, C/C back F/S, Carbon Aerogel insulation, C/C radiation shield and the C/C close-out were constructed based on the analytical temperature predictions presented in Part One of this work.
Mars entry vehicle↗