NASA’s Artemis II mission, set to launch astronauts around the Moon, has drawn particular attention to the thermal protection system on the Orion spacecraft, especially the heat shield that protects the crew module during reentry. This heat shield uses AVCOAT ablative material, which is designed to absorb and carry heat away as it erodes during the intense atmospheric return phase. After the uncrewed Artemis I flight, post-flight inspections revealed unexpected charring and material loss on the heat shield, prompting NASA engineers to analyze the thermal performance of the shield in more detail and reassess their confidence in its ability to protect astronauts on Artemis II.

To address these concerns, NASA has conducted thermal analyses, simulations, and additional testing of the shield material and reentry conditions, combining ground-based heat-flux testing with reentry-trajectory modeling to evaluate how the shield responds to the intense thermal environment. Rather than replacing the shield entirely, NASA adjusted the planned reentry trajectory to a steeper angle — a change that reduces the total heating exposure time on the shield material. Engineers argue that this modification, backed by their thermal modeling and tests, will keep the capsule’s peak temperatures and ablation within safe limits, protecting both structure and crew.

NASA and the Artemis II astronauts have publicly expressed confidence in the shield’s performance based on this body of thermal testing and analysis, even as some critics have argued that the unexpected erosion seen on the Orion heat shield during Artemis I underlines the inherent risks of reentry heat loading at lunar-return velocities. NASA’s review and test programs aimed to ensure that the shield’s thermal protection margins are sufficient for the upcoming crewed mission while continuing to refine future heat-shield designs for Artemis III and beyond.