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NASA-LLIS-0421
Lessons Learned – Voyager II Instrument Boom Deployment Anomaly (1977)
Year: 1996
Abstract: Abstract:
The Voyager II Science Boom failed to indicate, by microswitch, that it had deployed completely. The design of deployment mechanisms should consider susceptibility to jamming by foreign objects. Deployment clearance verification testing should be repeated if any related changes are incorporated.
The Voyager II Science Boom failed to indicate, by microswitch, that it had deployed completely. The design of deployment mechanisms should consider susceptibility to jamming by foreign objects. Deployment clearance verification testing should be repeated if any related changes are incorporated.
Subject: Hardware
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:39:05Z | |
| date available | 2017-09-04T16:39:05Z | |
| date copyright | 07/08/1996 | |
| date issued | 1996 | |
| identifier other | VKBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/102685 | |
| description abstract | Abstract: The Voyager II Science Boom failed to indicate, by microswitch, that it had deployed completely. The design of deployment mechanisms should consider susceptibility to jamming by foreign objects. Deployment clearance verification testing should be repeated if any related changes are incorporated. | |
| language | English | |
| title | NASA-LLIS-0421 | num |
| title | Lessons Learned – Voyager II Instrument Boom Deployment Anomaly (1977) | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1996 | |
| contenttype | fulltext | |
| subject keywords | Hardware | |
| subject keywords | Spacecraft | |
| subject keywords | Test & Verification |