NASA-LLIS-0705
Lessons Learned – Micrometeoroid Protection
Year: 2000
Abstract: Abstract:
Preferred Practice for Design & Test. The absence of micrometeoroid protection measures in spacecraft and mission design will increase the risk of significant damage to the spacecraft, particularly in areas of high meteoroid flux and during vulnerable mission phases.
Provide protection for the spacecraft structure and instruments to minimize damage from micrometeoroid penetration. Typical reliability engineering measures range from structural positioning to protect sensitive hardware to placement of protective blankets on the spacecraft exterior.
Preferred Practice for Design & Test. The absence of micrometeoroid protection measures in spacecraft and mission design will increase the risk of significant damage to the spacecraft, particularly in areas of high meteoroid flux and during vulnerable mission phases.
Provide protection for the spacecraft structure and instruments to minimize damage from micrometeoroid penetration. Typical reliability engineering measures range from structural positioning to protect sensitive hardware to placement of protective blankets on the spacecraft exterior.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:00:58Z | |
| date available | 2017-09-04T17:00:58Z | |
| date copyright | 03/16/2000 | |
| date issued | 2000 | |
| identifier other | XQCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/124467 | |
| description abstract | Abstract: Preferred Practice for Design & Test. The absence of micrometeoroid protection measures in spacecraft and mission design will increase the risk of significant damage to the spacecraft, particularly in areas of high meteoroid flux and during vulnerable mission phases. Provide protection for the spacecraft structure and instruments to minimize damage from micrometeoroid penetration. Typical reliability engineering measures range from structural positioning to protect sensitive hardware to placement of protective blankets on the spacecraft exterior. | |
| language | English | |
| title | NASA-LLIS-0705 | num |
| title | Lessons Learned – Micrometeoroid Protection | en |
| type | standard | |
| page | 9 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |

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