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NASA-LLIS-0707
Lessons Learned – Fault Tolerant Design
Year: 2000
Abstract: Practice:
Incorporate hardware and software features in the design of spacecraft equipment which tolerate the effects of minor failures and minimize switching from the primary to the secondary string. This increases the potential availability and reliability of the primary string.
Incorporate hardware and software features in the design of spacecraft equipment which tolerate the effects of minor failures and minimize switching from the primary to the secondary string. This increases the potential availability and reliability of the primary string.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:14:07Z | |
| date available | 2017-09-04T15:14:07Z | |
| date copyright | 03/16/2000 | |
| date issued | 2000 | |
| identifier other | ARCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/12879 | |
| description abstract | Practice: Incorporate hardware and software features in the design of spacecraft equipment which tolerate the effects of minor failures and minimize switching from the primary to the secondary string. This increases the potential availability and reliability of the primary string. | |
| language | English | |
| title | NASA-LLIS-0707 | num |
| title | Lessons Learned – Fault Tolerant Design | en |
| type | standard | |
| page | 5 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |