NASA-LLIS-0092
Lessons Learned - Spent Booster Segment Handling Operation
Year: 1992
Abstract: Description of Driving Event:
During forward center segment on-load to rail car for transport to the furbishment facility, the segment began to slide out of the confines of the handling sling. Approximately 90% of the segment was suspended 10' to 15' feet above the rail car when the aft end of the segment slipped out of the sling, coming to rest on the rail car. The forward end of the segment stayed suspended approximately 10' above the rail car. No damage to the segment was noted and the rail car received only three scratches by the handling ring. The instability of the segment is due to the difficulty in determining its center of gravity.
During forward center segment on-load to rail car for transport to the furbishment facility, the segment began to slide out of the confines of the handling sling. Approximately 90% of the segment was suspended 10' to 15' feet above the rail car when the aft end of the segment slipped out of the sling, coming to rest on the rail car. The forward end of the segment stayed suspended approximately 10' above the rail car. No damage to the segment was noted and the rail car received only three scratches by the handling ring. The instability of the segment is due to the difficulty in determining its center of gravity.
Subject: Flight Equipment
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:26:41Z | |
| date available | 2017-09-04T17:26:41Z | |
| date copyright | 07/28/1992 | |
| date issued | 1992 | |
| identifier other | CKYCQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/149812 | |
| description abstract | Description of Driving Event: During forward center segment on-load to rail car for transport to the furbishment facility, the segment began to slide out of the confines of the handling sling. Approximately 90% of the segment was suspended 10' to 15' feet above the rail car when the aft end of the segment slipped out of the sling, coming to rest on the rail car. The forward end of the segment stayed suspended approximately 10' above the rail car. No damage to the segment was noted and the rail car received only three scratches by the handling ring. The instability of the segment is due to the difficulty in determining its center of gravity. | |
| language | English | |
| title | NASA-LLIS-0092 | num |
| title | Lessons Learned - Spent Booster Segment Handling Operation | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1992 | |
| contenttype | fulltext | |
| subject keywords | Flight Equipment | |
| subject keywords | Flight Operations | |
| subject keywords | Launch Process | |
| subject keywords | Launch Vehicle | |
| subject keywords | Lifting Devices | |
| subject keywords | Pressure Vessels | |
| subject keywords | Transportation |

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