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A SpaceX Falcon 9 rocket launched the ninth Dragon spacecraft on the seventh operational cargo delivery mission to the International Space Station as part of the NASA cargo resupply contract. It was meant to deliver the IDA-1 segment of the new ISS International Docking System. The second stage ruptured due to an overpressurization event and the launch vehicle disintegrated at T+139 seconds. According to SpaceX investigation, "Preliminary analysis suggests the overpressure event in the upper stage liquid oxygen tank was initiated by a flawed piece of support hardware (a “strutâ€) inside the second stage."
RUD at T + 139s - second stage overpressure event due to defective COPV strut heim joint
This vehicle was intended to deliver the first of two International Docking Adapters to modify the ISS adapters so that they could be used for future commercial crew missions. However the capsule was destroyed when the Falcon 9 launch vehicle failed in flight.
Limiting rule: No flight through a thick (>4500 ft) cloud layer extending across the freezing level.
max-top 7900 m, mean 5507 m, 100% cover, freezing 5054 m · max cloud-top 7900 m above freezing 5054 m (100% cover in 10 nmi) · no GLM flashes within 25 nmi / 30 min, likely cirrus / stratiform ice rather than cumulus