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 |