درباره ما
NASA-LLIS-0774
Lessons Learned - Electrical Isolation Verification (DC)
Year: 2000
Abstract: Practice:
Direct current (DC) electrical isolation verification tests are made as part of the EMC test of hardware prior to final spacecraft assembly. Flight acceptance isolation retest is required after any hardware rework of subsystems with electrical interfaces that utilize system wiring.
Direct current (DC) electrical isolation verification tests are made as part of the EMC test of hardware prior to final spacecraft assembly. Flight acceptance isolation retest is required after any hardware rework of subsystems with electrical interfaces that utilize system wiring.
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:23:08Z | |
| date available | 2017-09-04T17:23:08Z | |
| date copyright | 04/11/2000 | |
| date issued | 2000 | |
| identifier other | ZYCEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/146342 | |
| description abstract | Practice: Direct current (DC) electrical isolation verification tests are made as part of the EMC test of hardware prior to final spacecraft assembly. Flight acceptance isolation retest is required after any hardware rework of subsystems with electrical interfaces that utilize system wiring. | |
| language | English | |
| title | NASA-LLIS-0774 | num |
| title | Lessons Learned - Electrical Isolation Verification (DC) | en |
| type | standard | |
| page | 6 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |