The Artemis II mission, which carried four astronauts around the Moon and back to Earth, marked the first crewed test of the Orion spacecraft. NASA said the thermal protection system effectively safeguarded the crew and spacecraft systems during reentry into Earth's atmosphere. Orion reached a maximum velocity of 39 times the speed of sound and experienced external temperatures exceeding 4,000 degrees Fahrenheit, while the cabin remained in the mid-70 degree Fahrenheit range.
After extensive arc jet testing at NASA's Ames Research Center, the agency modified Orion's reentry trajectory for Artemis II by shortening the maximum downrange distance between atmospheric entry and splashdown in the Pacific Ocean. This change limited the time the heat shield spent in the temperature range where the Artemis I heat shield phenomenon occurred. The analysis confirmed initial data from the mission and builds on NASA's earlier identification of the cause of char loss on the Artemis I heat shield.