On 28 January 1986, the Space Shuttle Challenger broke apart, 73 seconds into flight. All seven crew members died. The cause of the disaster was the failure of an O-ring on the right solid rocket booster. (O-rings help seal the joints of different segments of the solid rocket boosters.) It is now known that a leading factor in the O-ring failure was the exceptionally low temperature (about 31° F) at the time of the launch.
The table below gives the temperature (in ° F) at launch and O-ring erosion (in mils) for 22 solid rocket boosters, and is adapted from Reference [1].
Temperature | Erosion |
---|---|
66.0 | 0.0 |
70.0 | 53.0 |
69.0 | 0.0 |
68.0 | 0.0 |
67.0 | 0.0 |
72.0 | 0.0 |
73.0 | 0.0 |
70.0 | 0.0 |
57.0 | 40.0 |
63.0 | 0.0 |
70.0 | 28.0 |
78.0 | 0.0 |
67.0 | 0.0 |
53.0 | 48.0 |
67.0 | 0.0 |
75.0 | 0.0 |
70.0 | 0.0 |
81.0 | 0.0 |
76.0 | 0.0 |
79.0 | 0.0 |
75.0 | 0.0 |
76.0 | 0.0 |
The table below gives the temperature (again in ° F) and O-ring damage index for 23 Space Shuttle launches, and is adapted from Reference [2]. The damage index is a severity-weighted total number of incidents of O-ring erosion, heating, and blow-by.
Temperature | Index |
---|---|
53 | 11 |
57 | 4 |
58 | 4 |
63 | 2 |
66 | 0 |
67 | 0 |
67 | 0 |
67 | 0 |
68 | 0 |
69 | 0 |
70 | 4 |
70 | 0 |
70 | 4 |
70 | 0 |
72 | 0 |
73 | 0 |
75 | 0 |
75 | 4 |
76 | 0 |
76 | 0 |
78 | 0 |
79 | 0 |
81 | 0 |