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NASA-LLIS-0700
Lessons Learned - Fracture Mechanics Reliability
Year: 2000
Abstract: Practice:
Use a fracture mechanics formulation to estimate the design fatigue life and reliability of metallic or ceramic structural and mechanical components subject to fluctuating stress. For reusable spacecraft, update the reliability analysis based on in-service inspection and repair data.
Use a fracture mechanics formulation to estimate the design fatigue life and reliability of metallic or ceramic structural and mechanical components subject to fluctuating stress. For reusable spacecraft, update the reliability analysis based on in-service inspection and repair data.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:34:36Z | |
| date available | 2017-09-04T15:34:36Z | |
| date copyright | 03/15/2000 | |
| date issued | 2000 | |
| identifier other | ONCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/36392 | |
| description abstract | Practice: Use a fracture mechanics formulation to estimate the design fatigue life and reliability of metallic or ceramic structural and mechanical components subject to fluctuating stress. For reusable spacecraft, update the reliability analysis based on in-service inspection and repair data. | |
| language | English | |
| title | NASA-LLIS-0700 | num |
| title | Lessons Learned - Fracture Mechanics Reliability | en |
| type | standard | |
| page | 9 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |