This approach essentially reverse artimes' approach (shallow, longer, skip-like descent) to Apollo's approach (steeper, shorter, ballistic descent). Funny thing is that Artimes uses Apollo's heatshield material and ends up in the same descending profile.Long story short, they launched an investigation into the Artemis I heatshield and found that during reentry, gases generated inside the Avcoat (the shield's ablative material) could not vent properly which caused pressure to build up, leading to cracking of charred chunks but well within margins. They are adjusting Orion's reentry profile for Artemis II to a steeper angle to reduce the dwell time at altitudes where this outgassing occurs, so it will spend about 8 minutes rather than the 15 minutes in these conditions.

