NASA-LLIS-0371
Lessons Learned - SEASAT Failure
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:28:35Z | |
| date available | 2017-09-04T18:28:35Z | |
| date copyright | 01/24/1995 | |
| date issued | 1995 | |
| identifier other | IRAEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho146/handle/yse/210713 | |
| description abstract | Abstract: The SEASAT Spacecraft failed in orbit due to arcing between adjacent slip ring brush assemblies. It was discovered that the Agena bus had been substantially modified, but were treated as a heritage design not requiring requalification. Plans should be made early in the project to fully evaluate the heritage of previously used equipment. When conducting a FMECA on electrical components, electrical short failure modes should be considered. | |
| language | English | |
| title | NASA-LLIS-0371 | num |
| title | Lessons Learned - SEASAT Failure | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1995 | |
| contenttype | fulltext | |
| subject keywords | Hardware | |
| subject keywords | Inherited Equipment | |
| subject keywords | Slip Rings |

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