Challenger Shuttle Crash Case Study

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Case Study Analysis Activity Title: Name: Date: Cause(s) of Accident The Challenger shuttle crash was a crash that touched the hearts of every American due to the televised coverage and the relate ability of the crew. There was concern from the engineers that the unusually cold weather the morning of the launch could have adverse affects on the rubber O-rings that sealed the joints of the shuttles solid rocket boosters. The cold weather on the morning of January 28, 1986 caused the O-rings to tear and leak fuel from the boosters. (Dunbar B, 2005) Structural and Mechanical Factors The investigation discovered that the cold weather affected the plasticity of the O-rings that sealed the solid rocket boosters, the O-rings where not designed …show more content…

Some of the earlier tests of the seals brought to the attention of the engineers that the seals where prone to failure when exposed to extreme temptures and due to the location of the seals not staying within the parameters of the seals would cause a catastrophic failure. Other warnings where not taken into account when the launch days drew closer, the unusually cold weather caused delays in the original launch date and the on the new launch day the temtures around the seals where estimated “to be 28degrees +/- 5 degrees Fahrenheit” (NASA, n.d). According to the NASA investigation …show more content…

The failure was due to a faulty design unacceptably sensitive to a number of factors. (NASA, n/d) Recommendations They’re where a lot of purposed recommendations from the commission to help ensure that any future shuttle missions would not experience the same catastrophic O-ring failure like the challenger shuttle. The first recommendation was to redesign the O-ring by improving “structural capability, seal redundancy, and thermal protection” (NASA, n/d). This change would also redesign the tang and clevis of the mating points of the rocket. The redesign not only used a third O-ring seal but also a newly redesigned “O-ring seals are designed to not leak under structural deflection of twice the expected values” (NASA, n/d) Outcomes The panel has held a number of full meetings and numerous subpanel and individual member meetings, and has submitted three written status reports to the NASA Administrator. Although NASA has not yet formally responded to these status reports, actions have been taken to implement most of the committee recommendations. NASA has held several meetings with the committee to discuss and review the status of the response to the recommendations. The NRC membership and a summary of the panel responsibilities are provided in Appendix

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