Second Stage Engine Cutoff Delayed by 27 Seconds Post-Launch
The second stage engine cutoff of a recent launch was delayed by 27 seconds, with the subsequent ignition also postponed by 15 seconds and ending shortly after initiation. Telemetry data revealed a drop in hydrogen tank pressure during the first-stage burn, leading to an investigation into the anomaly.

Following the launch, it was reported that the first second stage engine cutoff occurred 27 seconds later than intended. Additionally, the second ignition was delayed by 15 seconds and terminated almost immediately after startup. Telemetry data indicated that hydrogen tank pressure in the second stage began to fall during the first-stage burn, prompting an investigation into the anomaly.




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