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 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.