What have we learned from the Artemis II mission?
The SLS generated 8.8 million pounds of thrust at liftoff and, by every measure engineers care about, performed to plan. Each phase of the ascent was, in the understated language of mission control, “nominal”: maximum dynamic pressure, main engine cut-off and booster separation.
The SLS generated 8.8 million pounds of thrust at liftoff and, by every measure engineers care about, performed to plan. Each phase of the ascent was, in the understated language of mission control, “nominal”: maximum dynamic pressure, main engine cut-off and booster separation.
