KSC-05-S-00093

Launch Team: The vehicle max-q. Launch Team: Attitude nominal. The vehicle fin actuator system, which is used to control vehicle attitude during stage one burn, is performing properly. Launch Team: Attitude is nominal, vehicle power buses remain strong. Launch Team: (various) Launch Team: And traveling at 4,000 miles per hour. Launch Team: Attitude remains nominal. Launch Team: Attitude and power remain nominal. Launch Team: Maximum aerodynamic heating. Stage one burnout. Launch Team: This picture coming from Peak. Correction, Santa Ynez Mountain. Santa Ynez tracker. Launch Team: Stage two TVC battery on. Voltage and currance and status nominal. Launch Team: Stage one separation. Launch Team: Stage one separation. Launch Team: Stage two ignition. Launch Team: Stage two ignition. Launch Team: (various) Launch Team: Vehicle is past 50 miles in altitude. Attitude is nominal. Launch Team: Attitude remains nominal. Launch Team: All buses strong. Two minutes into the DART mission, all systems nominal. George Diller: In this video coming from the tracker, between Santa Barbara and Vandenberg Air Force Base. Launch Team: Motor pressures are nominal. We have fairing separation. Launch Team: Fairing separation. Launch Team: Attitude nominal. Power buses strong. Launch Team: Attitude is nominal. Launch Team: GPS has switched the stage three antenna. Launch Team: And we have safe five op on the stage three antenna. FTS system remains nominal. Attitude remains nominal. Launch Team: Attitude remains nominal. Launch Team: Stage two burnout. Attitude is nominal. Launch Team: Stage two burnout. Launch Team: Pegasus is now in a stage two-three coast phase. Launch Team: And they're in the coast phase.