Spacecraft reflectors thermomechanical analysis
In this article, thermo-mechanical analysis results of the composite reflectors for the use on the geostationary Earth orbit possibility studies are described. The behavior of two different space reflector structures manufactured on composite materials is investigated. The estimates of reflecting su...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
EDP Sciences
2015-01-01
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| Series: | EPJ Web of Conferences |
| Online Access: | http://dx.doi.org/10.1051/epjconf/20158201005 |
| _version_ | 1818778810256982016 |
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| author | Ponomarev Viktor S. Gerasimov Alexander V. Ponomarev Sergey V. Shendalev Denis O. |
| author_facet | Ponomarev Viktor S. Gerasimov Alexander V. Ponomarev Sergey V. Shendalev Denis O. |
| author_sort | Ponomarev Viktor S. |
| collection | DOAJ |
| description | In this article, thermo-mechanical analysis results of the composite reflectors for the use on the geostationary Earth orbit possibility studies are described. The behavior of two different space reflector structures manufactured on composite materials is investigated. The estimates of reflecting surfaces RMS deviations for the two extreme cases orbital inclinations are presented. |
| first_indexed | 2024-12-18T11:50:38Z |
| format | Article |
| id | doaj.art-56903b1d21e64dc09ef933b3fe52ba46 |
| institution | Directory Open Access Journal |
| issn | 2100-014X |
| language | English |
| last_indexed | 2024-12-18T11:50:38Z |
| publishDate | 2015-01-01 |
| publisher | EDP Sciences |
| record_format | Article |
| series | EPJ Web of Conferences |
| spelling | doaj.art-56903b1d21e64dc09ef933b3fe52ba462022-12-21T21:09:10ZengEDP SciencesEPJ Web of Conferences2100-014X2015-01-01820100510.1051/epjconf/20158201005epjconf-tbet2014_01005Spacecraft reflectors thermomechanical analysisPonomarev Viktor S.Gerasimov Alexander V.Ponomarev Sergey V.0Shendalev Denis O.1Scientific Research Institute of Applied Mathematics and Mechanics of Tomsk State UniversityThe JSC “Academician M.F. Reshetnev “Information Satellite Systems”, ZheleznogorskIn this article, thermo-mechanical analysis results of the composite reflectors for the use on the geostationary Earth orbit possibility studies are described. The behavior of two different space reflector structures manufactured on composite materials is investigated. The estimates of reflecting surfaces RMS deviations for the two extreme cases orbital inclinations are presented.http://dx.doi.org/10.1051/epjconf/20158201005 |
| spellingShingle | Ponomarev Viktor S. Gerasimov Alexander V. Ponomarev Sergey V. Shendalev Denis O. Spacecraft reflectors thermomechanical analysis EPJ Web of Conferences |
| title | Spacecraft reflectors thermomechanical analysis |
| title_full | Spacecraft reflectors thermomechanical analysis |
| title_fullStr | Spacecraft reflectors thermomechanical analysis |
| title_full_unstemmed | Spacecraft reflectors thermomechanical analysis |
| title_short | Spacecraft reflectors thermomechanical analysis |
| title_sort | spacecraft reflectors thermomechanical analysis |
| url | http://dx.doi.org/10.1051/epjconf/20158201005 |
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