NASA-LLIS-0412
Lessons Learned – Voyager-Power Subsystem Coded Commands Interface with the Computer Command Subsystem (CCS) (~1975)
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:58:24Z | |
| date available | 2017-09-04T16:58:24Z | |
| date copyright | 06/26/1996 | |
| date issued | 1996 | |
| identifier other | XJBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/121783 | |
| description abstract | Abstract: Because, the interface circuit between the Voyager CCS and Power subsystems was not electrically isolated, spacecraft system noise prevented reliable commanding from CCS to Power. This was not discovered until system-level test, and circuit modifications were difficult. Lesson recommendations pertain to system level requirements, design, and early compatibility testing for interface circuits. | |
| language | English | |
| title | NASA-LLIS-0412 | num |
| title | Lessons Learned – Voyager-Power Subsystem Coded Commands Interface with the Computer Command Subsystem (CCS) (~1975) | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1996 | |
| contenttype | fulltext | |
| subject keywords | Electrical Isolations | |
| subject keywords | Spacecraft | |
| subject keywords | Test & Verification |

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