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NASA-LLIS-0799
Lessons Learned – Redundancy Switching Analysis
Year: 2000
Abstract: Practice:
To verify that the failure of one of two redundant functions does not impair the ability to transfer to the second function, a rigorous failure modes, effects, and criticality analysis (FMECA) at the piece part-level is performed for all interfacing circuits.
To verify that the failure of one of two redundant functions does not impair the ability to transfer to the second function, a rigorous failure modes, effects, and criticality analysis (FMECA) at the piece part-level is performed for all interfacing circuits.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:04:12Z | |
| date available | 2017-09-04T17:04:12Z | |
| date copyright | 04/17/2000 | |
| date issued | 2000 | |
| identifier other | XZCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/127805 | |
| description abstract | Practice: To verify that the failure of one of two redundant functions does not impair the ability to transfer to the second function, a rigorous failure modes, effects, and criticality analysis (FMECA) at the piece part-level is performed for all interfacing circuits. | |
| language | English | |
| title | NASA-LLIS-0799 | num |
| title | Lessons Learned – Redundancy Switching Analysis | en |
| type | standard | |
| page | 5 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |