NASA-LLIS-0436
Lessons Learned - Receiver 1 Power Converter Failure on Voyager 2 (1978)
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:30:30Z | |
| date available | 2017-09-04T16:30:30Z | |
| date copyright | 07/17/1996 | |
| date issued | 1996 | |
| identifier other | UMBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/93855 | |
| description abstract | Abstract: A Voyager telemetry failure was attributed to over-length screws that caused conductive end-caps to contact areas not sufficiently coated by conformal coating. The lesson provides recommendations for design of captivated inserts, QA monitoring of assembly, application of conformal coatings, and planning of ground activities. | |
| language | English | |
| title | NASA-LLIS-0436 | num |
| title | Lessons Learned - Receiver 1 Power Converter Failure on Voyager 2 (1978) | en |
| type | standard | |
| page | 4 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1996 | |
| contenttype | fulltext | |
| subject keywords | Captive Inserts | |
| subject keywords | Conformal Coatings | |
| subject keywords | Hardware | |
| subject keywords | Mission Operations | |
| subject keywords | Parts Materials & Processes | |
| subject keywords | Surveillance |

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