NASA-LLIS-0708
Lessons Learned – Plasma Noise in EMI Design
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:22:08Z | |
| date available | 2017-09-04T15:22:08Z | |
| date copyright | 03/16/2000 | |
| date issued | 2000 | |
| identifier other | NBDEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/22158 | |
| description abstract | Practice: Missions with payloads that can interact strongly with the ambient plasma, such as a high power electron beam, a high power RF source, or an ion engine, may require a structural current test for conducted susceptibility and higher radiated susceptibility test levels. The practice is to perform an analysis early in such a program to estimate the amplitude of plasma noise induced electromagnetic interference (EMI). This may identify potential adverse effects on operational reliability. | |
| language | English | |
| title | NASA-LLIS-0708 | num |
| title | Lessons Learned – Plasma Noise in EMI Design | en |
| type | standard | |
| page | 4 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |

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