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NASA-LLIS-0409
Lessons Learned - Voyager Gyro Swap During Launch Phase (1977)
Year: 1996
Abstract: Abstract:
Because the Voyager 2 failure protection logic was unnecessarily enabled during launch, transient gyro outputs triggered a series of alarming "gyro swaps." Careful attention should be given to preclude the possibility of spurious inputs triggering unwanted events when the protection logic is enabled.
Because the Voyager 2 failure protection logic was unnecessarily enabled during launch, transient gyro outputs triggered a series of alarming "gyro swaps." Careful attention should be given to preclude the possibility of spurious inputs triggering unwanted events when the protection logic is enabled.
Subject: Flight Equipment
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:03:57Z | |
| date available | 2017-09-04T16:03:57Z | |
| date copyright | 06/24/1996 | |
| date issued | 1996 | |
| identifier other | RSBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/67302 | |
| description abstract | Abstract: Because the Voyager 2 failure protection logic was unnecessarily enabled during launch, transient gyro outputs triggered a series of alarming "gyro swaps." Careful attention should be given to preclude the possibility of spurious inputs triggering unwanted events when the protection logic is enabled. | |
| language | English | |
| title | NASA-LLIS-0409 | num |
| title | Lessons Learned - Voyager Gyro Swap During Launch Phase (1977) | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1996 | |
| contenttype | fulltext | |
| subject keywords | Flight Equipment | |
| subject keywords | Spacecraft |