D-10, 9, 8, 7, 6, 5, 4, 3, 2, 1. Ignition, lift off of Aries 1X, testing concepts for the future of new rocket design. The altitude now 2 miles. Paper pressure now tapering off as the side vehicles lining the line itself with the plant trajectory. We passed Mach 1 and we're now passing Max Q. We have our Max Q system ID, maneuver PTI engaged. Solid motor chamber pressure picking up again. P plus 62 seconds. Now passing Mach 2, vehicle now 10 miles altitude downrange distance 8 miles and velocity of 1540 miles per hour. Plus 80 seconds we started our supersonic large altitude ID, maneuver PTI. We see the response. And we started the last PTI maneuver, structural mode ID. And we passed T plus 1 whole 105 seconds. People's now traveling Mach 4, 20 miles altitude downrange distance 32 miles. The SRM tail off is observed. Burn out. Our APUs of shutdown, CRDs of shutdown, medium fire, and SEP. We show SEP and a tumble motor ignition. And we can also confirm on video. We see both parts of the vehicle tumbling, the first stage as well as the upper stage, successful separation, clean signal all the way. T plus 150 seconds. And we'll have a burnout, orbit parameter in just a second. These numbers were calculated right at burnout. They height of apogee 21.92.