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NASA-LLIS-0389
Lessons Learned - In-Flight Power Converter Failure
Year: 1995
Abstract: Abstract:
During a switch between Voyager radio receivers, a failure occurred due to a short circuit traced to a screw contacting components insufficiently coated by the solithane conformal coating. Designers should be aware of tolerance build-up in assemblies and assure that there is adequate margin.
During a switch between Voyager radio receivers, a failure occurred due to a short circuit traced to a screw contacting components insufficiently coated by the solithane conformal coating. Designers should be aware of tolerance build-up in assemblies and assure that there is adequate margin.
Subject: Spacecraft
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:04:28Z | |
| date available | 2017-09-04T18:04:28Z | |
| date copyright | 03/13/1995 | |
| date issued | 1995 | |
| identifier other | GHBEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/187415 | |
| description abstract | Abstract: During a switch between Voyager radio receivers, a failure occurred due to a short circuit traced to a screw contacting components insufficiently coated by the solithane conformal coating. Designers should be aware of tolerance build-up in assemblies and assure that there is adequate margin. | |
| language | English | |
| title | NASA-LLIS-0389 | num |
| title | Lessons Learned - In-Flight Power Converter Failure | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1995 | |
| contenttype | fulltext | |
| subject keywords | Spacecraft |