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NASA-LLIS-0188
Lessons Learned - T-0 Umbilical Carrier Plate.
Year: 1992
Abstract: Description of Driving Event:
As a result of lower release mechanism pin hole elongation, there is potential for premature disconnect of the T-0 umbilical carrier plate due to failure of the LO2/LH2 tail service mast (TSM) lower release mechanism pin hole structure to support the dropweight.
As a result of lower release mechanism pin hole elongation, there is potential for premature disconnect of the T-0 umbilical carrier plate due to failure of the LO2/LH2 tail service mast (TSM) lower release mechanism pin hole structure to support the dropweight.
Subject: Ground Equipment
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:59:38Z | |
| date available | 2017-09-04T15:59:38Z | |
| date copyright | 33906 | |
| date issued | 1992 | |
| identifier other | RFZCQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/62783 | |
| description abstract | Description of Driving Event: As a result of lower release mechanism pin hole elongation, there is potential for premature disconnect of the T-0 umbilical carrier plate due to failure of the LO2/LH2 tail service mast (TSM) lower release mechanism pin hole structure to support the dropweight. | |
| language | English | |
| title | NASA-LLIS-0188 | num |
| title | Lessons Learned - T-0 Umbilical Carrier Plate. | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1992 | |
| contenttype | fulltext | |
| subject keywords | Ground Equipment | |
| subject keywords | Ground Operations | |
| subject keywords | Launch Process |