SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT
Usually satellite is under complex dynamic load during the launch phase,it’s easy to cause satellitestructure damageto influence spacecraftmission. Mechanical environment tests show that spacecraftstructure damage always occurs because of larger acceleration response of equipment such as large mass...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2019-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.01.006 |
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| _version_ | 1841535641701056512 |
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| author | ZHAO Hua YU Kuai Fan Ning |
| author_facet | ZHAO Hua YU Kuai Fan Ning |
| author_sort | ZHAO Hua |
| collection | DOAJ |
| description | Usually satellite is under complex dynamic load during the launch phase,it’s easy to cause satellitestructure damageto influence spacecraftmission. Mechanical environment tests show that spacecraftstructure damage always occurs because of larger acceleration response of equipment such as large mass or high center of mass,and affecttedthe project development.Difference from the usual engineering solutions,a method based on gap elastic impactting is studiedto reducing damage. By constructing mechanical model,simulation and analysis has been done to a designated parameter structurepanel and equipment,results show that the methed as one of solutions of lower damage is valid to reducing defomation and load located at connection between equipment andstructure. |
| format | Article |
| id | doaj-art-a217bdf13f5842c59d1c182ad7b96a5f |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2019-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-a217bdf13f5842c59d1c182ad7b96a5f2025-01-15T02:30:29ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692019-01-0141333830603634SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACTZHAO HuaYU KuaiFan NingUsually satellite is under complex dynamic load during the launch phase,it’s easy to cause satellitestructure damageto influence spacecraftmission. Mechanical environment tests show that spacecraftstructure damage always occurs because of larger acceleration response of equipment such as large mass or high center of mass,and affecttedthe project development.Difference from the usual engineering solutions,a method based on gap elastic impactting is studiedto reducing damage. By constructing mechanical model,simulation and analysis has been done to a designated parameter structurepanel and equipment,results show that the methed as one of solutions of lower damage is valid to reducing defomation and load located at connection between equipment andstructure.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.01.006Satellite structureAcceleration responseDamageImpact limitamplitudeStimulationReduce damage failure |
| spellingShingle | ZHAO Hua YU Kuai Fan Ning SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT Jixie qiangdu Satellite structure Acceleration response Damage Impact limitamplitude Stimulation Reduce damage failure |
| title | SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT |
| title_full | SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT |
| title_fullStr | SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT |
| title_full_unstemmed | SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT |
| title_short | SATELLITESTRUCTURE REDUCING DAMAGE RESEARCHAND STIMULATION BASEDON ELASTIC IMPACT |
| title_sort | satellitestructure reducing damage researchand stimulation basedon elastic impact |
| topic | Satellite structure Acceleration response Damage Impact limitamplitude Stimulation Reduce damage failure |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.01.006 |
| work_keys_str_mv | AT zhaohua satellitestructurereducingdamageresearchandstimulationbasedonelasticimpact AT yukuai satellitestructurereducingdamageresearchandstimulationbasedonelasticimpact AT fanning satellitestructurereducingdamageresearchandstimulationbasedonelasticimpact |