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NASA-LLIS-0697
Lessons Learned – Active Redundancy
Year: 2000
Abstract: Practice:
Use active redundancy as a design option when development testing and reliability analysis show that a single component is not reliable enough to accomplish the function. Although active redundancy can be applied to various types of mechanical and electrical components and systems, the application detailed in this practice illustrates an approach using a Traveling Wave Tube amplifier in a space flight application.
Use active redundancy as a design option when development testing and reliability analysis show that a single component is not reliable enough to accomplish the function. Although active redundancy can be applied to various types of mechanical and electrical components and systems, the application detailed in this practice illustrates an approach using a Traveling Wave Tube amplifier in a space flight application.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:56:48Z | |
| date available | 2017-09-04T17:56:48Z | |
| date copyright | 03/04/2000 | |
| date issued | 2000 | |
| identifier other | FNCEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/179868 | |
| description abstract | Practice: Use active redundancy as a design option when development testing and reliability analysis show that a single component is not reliable enough to accomplish the function. Although active redundancy can be applied to various types of mechanical and electrical components and systems, the application detailed in this practice illustrates an approach using a Traveling Wave Tube amplifier in a space flight application. | |
| language | English | |
| title | NASA-LLIS-0697 | num |
| title | Lessons Learned – Active Redundancy | en |
| type | standard | |
| page | 8 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |