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NASA-LLIS-1010
Lessons Learned – Space Shuttle Program/Super Light Weight External Tank/Materials & Test and Verification Changes
Year: 1997
Abstract: Description of Driving Event:
Lower than Anticipated Fracture Toughness of the 2195 Aluminum-Lithium Alloy Used in the SLWT at Cryogenic Temperatures Causing Changes to Test & Verification Procedures.
Lower than Anticipated Fracture Toughness of the 2195 Aluminum-Lithium Alloy Used in the SLWT at Cryogenic Temperatures Causing Changes to Test & Verification Procedures.
Subject: Aerospace Safety Advisory Panel
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:10:11Z | |
| date available | 2017-09-04T16:10:11Z | |
| date copyright | 02/01/1997 | |
| date issued | 1997 | |
| identifier other | SIUEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/73453 | |
| description abstract | Description of Driving Event: Lower than Anticipated Fracture Toughness of the 2195 Aluminum-Lithium Alloy Used in the SLWT at Cryogenic Temperatures Causing Changes to Test & Verification Procedures. | |
| language | English | |
| title | NASA-LLIS-1010 | num |
| title | Lessons Learned – Space Shuttle Program/Super Light Weight External Tank/Materials & Test and Verification Changes | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1997 | |
| contenttype | fulltext | |
| subject keywords | Aerospace Safety Advisory Panel | |
| subject keywords | Cryogenic Systems | |
| subject keywords | Energetic Materials - Explosive/Propellant/Pyrotechnic | |
| subject keywords | Hardware | |
| subject keywords | Parts Materials & Processes | |
| subject keywords | Policy & Planning | |
| subject keywords | Risk Management/Assessment | |
| subject keywords | Spacecraft | |
| subject keywords | Standard | |
| subject keywords | Test & Verification |