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NASA-LLIS-0400
Lessons Learned - Spacecraft Structure Dynamical Interaction with Attitude Control
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:50:47Z | |
| date available | 2017-09-04T15:50:47Z | |
| date copyright | 06/08/1995 | |
| date issued | 1995 | |
| identifier other | QIBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/53915 | |
| description abstract | Abstract: As Mariner 10 approached Venus encounter, an uncontrolled oscillation occurred due to spacecraft structural interaction with the Attitude Control Subsystem. The result was a severe consumption of control gas that would have caused failure of the mission had it continued. The recommendations center on design and operational measures to cope with subtle and complex dynamical interactions between the spacecraft structure and the ACS. | |
| language | English | |
| title | NASA-LLIS-0400 | num |
| title | Lessons Learned - Spacecraft Structure Dynamical Interaction with Attitude Control | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1995 | |
| contenttype | fulltext | |
| subject keywords | Flexible Body Analysis | |
| subject keywords | Flight Equipment | |
| subject keywords | Hardware | |
| subject keywords | Software | |
| subject keywords | Spacecraft |
