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NASA-LLIS-0107
Lessons Learned - LH2 Leakage at the 8" T-0 Flexhose QD/Interface
Year: 1992
Abstract: Description of Driving Event:
The 8 inch T-0 flexhose connects the tail service mast (TSM) with the LH2 carrier plate. Due to mechanical design the interface connection is very poor. The LO2 interface is identical and has experienced leakage in the past. Undetected leakage could cause a major fire resulting loss of life or vehicle.
The 8 inch T-0 flexhose connects the tail service mast (TSM) with the LH2 carrier plate. Due to mechanical design the interface connection is very poor. The LO2 interface is identical and has experienced leakage in the past. Undetected leakage could cause a major fire resulting loss of life or vehicle.
Subject: Energetic Materials - Explosive/Propellant/Pyrotechnic
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:59:20Z | |
| date available | 2017-09-04T17:59:20Z | |
| date copyright | 08/19/1992 | |
| date issued | 1992 | |
| identifier other | FTYCQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/182443 | |
| description abstract | Description of Driving Event: The 8 inch T-0 flexhose connects the tail service mast (TSM) with the LH2 carrier plate. Due to mechanical design the interface connection is very poor. The LO2 interface is identical and has experienced leakage in the past. Undetected leakage could cause a major fire resulting loss of life or vehicle. | |
| language | English | |
| title | NASA-LLIS-0107 | num |
| title | Lessons Learned - LH2 Leakage at the 8" T-0 Flexhose QD/Interface | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1992 | |
| contenttype | fulltext | |
| subject keywords | Energetic Materials - Explosive/Propellant/Pyrotechnic | |
| subject keywords | Fire Protection | |
| subject keywords | Flight Equipment | |
| subject keywords | Ground Equipment | |
| subject keywords | Launch Vehicle |