RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY
A kind of pyroshock reduction device of honeycomb sandwich plate is designed,which takes the impact as the research object when satellite deploys the solar array. The dynamic model of shock response and the key points in design are explained in detail from the view of vibration reduction. Spring ele...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2018-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.01.006 |
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| _version_ | 1841535422558109696 |
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| author | JIANG ShuYu GU Song CHEN ShanBo |
| author_facet | JIANG ShuYu GU Song CHEN ShanBo |
| author_sort | JIANG ShuYu |
| collection | DOAJ |
| description | A kind of pyroshock reduction device of honeycomb sandwich plate is designed,which takes the impact as the research object when satellite deploys the solar array. The dynamic model of shock response and the key points in design are explained in detail from the view of vibration reduction. Spring element was introduced to improve the honeycomb sandwich plate and its accessory structure,then,the shock characteristics of the system wartested. Dynamic response of satellite after setting the damping device was analyzed. The result indicates that the honeycomb sandwich plate on mounting plate can effectively reduce shock response,and meet the launching condition,so the design is reasonable. |
| format | Article |
| id | doaj-art-19b5f6785fe144c6bfe9f1fe15f185d5 |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2018-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-19b5f6785fe144c6bfe9f1fe15f185d52025-01-15T02:32:40ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692018-01-0140333830600551RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAYJIANG ShuYuGU SongCHEN ShanBoA kind of pyroshock reduction device of honeycomb sandwich plate is designed,which takes the impact as the research object when satellite deploys the solar array. The dynamic model of shock response and the key points in design are explained in detail from the view of vibration reduction. Spring element was introduced to improve the honeycomb sandwich plate and its accessory structure,then,the shock characteristics of the system wartested. Dynamic response of satellite after setting the damping device was analyzed. The result indicates that the honeycomb sandwich plate on mounting plate can effectively reduce shock response,and meet the launching condition,so the design is reasonable.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.01.006SatelliteSolar arrayPyroshock reductionHoneycomb sandwich plate |
| spellingShingle | JIANG ShuYu GU Song CHEN ShanBo RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY Jixie qiangdu Satellite Solar array Pyroshock reduction Honeycomb sandwich plate |
| title | RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY |
| title_full | RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY |
| title_fullStr | RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY |
| title_full_unstemmed | RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY |
| title_short | RESEARCH ON PYROSHOCK REDUCTION STRUCTURE WHEN MICRO SATELLITE DEPLOYS THE SOLAR ARRAY |
| title_sort | research on pyroshock reduction structure when micro satellite deploys the solar array |
| topic | Satellite Solar array Pyroshock reduction Honeycomb sandwich plate |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.01.006 |
| work_keys_str_mv | AT jiangshuyu researchonpyroshockreductionstructurewhenmicrosatellitedeploysthesolararray AT gusong researchonpyroshockreductionstructurewhenmicrosatellitedeploysthesolararray AT chenshanbo researchonpyroshockreductionstructurewhenmicrosatellitedeploysthesolararray |