Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment
One of the most important tasks of the Federal Space Program of Russia for the period until 2025 is the creation of spacecraft for remote sensing of the Earth. An integral part of the design of this class spacecraft is the determination of the parameters of the orbits that are most effective from th...
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| Format: | Article |
| Language: | English |
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Peoples’ Friendship University of Russia (RUDN University)
2020-12-01
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| Series: | RUDN Journal of Engineering Research |
| Subjects: | |
| Online Access: | http://journals.rudn.ru/engineering-researches/article/viewFile/25555/19014 |
| _version_ | 1811174092914556928 |
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| author | Mikhail A. Gorodetskii Konstantin V. Mikhaylovskiy |
| author_facet | Mikhail A. Gorodetskii Konstantin V. Mikhaylovskiy |
| author_sort | Mikhail A. Gorodetskii |
| collection | DOAJ |
| description | One of the most important tasks of the Federal Space Program of Russia for the period until 2025 is the creation of spacecraft for remote sensing of the Earth. An integral part of the design of this class spacecraft is the determination of the parameters of the orbits that are most effective from the standpoint of information content, energy supply and the duration of active existence. In orbital flight, the temperature state of spacecraft in a complex way varies in time and space. The inhomogeneous temperature field of the structural elements of spacecraft can cause shape distortion, which adversely affects the performance of targets. A technique for a comprehensive analysis and determination of the platform composite design parameters, which is part of the spacecraft for remote sensing of the Earth is proposed. The conditions of thermal loading for flight in a sun-synchronous orbit are considered and mathematical modeling of the operating conditions that ensure the effective operation of such spacecraft is performed. The results of modeling the thermal regime of options for composite platform designs are presented. The technique will be useful in determining the complex of orbital characteristics of the Earth remote sensing satellite at the stage of technical proposals. |
| first_indexed | 2024-04-10T17:58:39Z |
| format | Article |
| id | doaj.art-acf9b99abc024b93b58471ee78bfaf60 |
| institution | Directory Open Access Journal |
| issn | 2312-8143 2312-8151 |
| language | English |
| last_indexed | 2024-04-10T17:58:39Z |
| publishDate | 2020-12-01 |
| publisher | Peoples’ Friendship University of Russia (RUDN University) |
| record_format | Article |
| series | RUDN Journal of Engineering Research |
| spelling | doaj.art-acf9b99abc024b93b58471ee78bfaf602023-02-02T17:15:31ZengPeoples’ Friendship University of Russia (RUDN University)RUDN Journal of Engineering Research2312-81432312-81512020-12-0121315916510.22363/2312-8143-2020-21-3-159-16519703Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipmentMikhail A. Gorodetskii0Konstantin V. Mikhaylovskiy1Bauman Moscow State Technical University (National Research University of Technology)Bauman Moscow State Technical University (National Research University of Technology)One of the most important tasks of the Federal Space Program of Russia for the period until 2025 is the creation of spacecraft for remote sensing of the Earth. An integral part of the design of this class spacecraft is the determination of the parameters of the orbits that are most effective from the standpoint of information content, energy supply and the duration of active existence. In orbital flight, the temperature state of spacecraft in a complex way varies in time and space. The inhomogeneous temperature field of the structural elements of spacecraft can cause shape distortion, which adversely affects the performance of targets. A technique for a comprehensive analysis and determination of the platform composite design parameters, which is part of the spacecraft for remote sensing of the Earth is proposed. The conditions of thermal loading for flight in a sun-synchronous orbit are considered and mathematical modeling of the operating conditions that ensure the effective operation of such spacecraft is performed. The results of modeling the thermal regime of options for composite platform designs are presented. The technique will be useful in determining the complex of orbital characteristics of the Earth remote sensing satellite at the stage of technical proposals.http://journals.rudn.ru/engineering-researches/article/viewFile/25555/19014earth remote sensing spacecraftsolar-synchronous orbitpolymer composite materialsstress-strain state |
| spellingShingle | Mikhail A. Gorodetskii Konstantin V. Mikhaylovskiy Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment RUDN Journal of Engineering Research earth remote sensing spacecraft solar-synchronous orbit polymer composite materials stress-strain state |
| title | Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment |
| title_full | Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment |
| title_fullStr | Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment |
| title_full_unstemmed | Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment |
| title_short | Development of a design methodology for heat-loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the Earth space equipment |
| title_sort | development of a design methodology for heat loaded dimensionally stable elements of carbon plastic construction for a remote sensing of the earth space equipment |
| topic | earth remote sensing spacecraft solar-synchronous orbit polymer composite materials stress-strain state |
| url | http://journals.rudn.ru/engineering-researches/article/viewFile/25555/19014 |
| work_keys_str_mv | AT mikhailagorodetskii developmentofadesignmethodologyforheatloadeddimensionallystableelementsofcarbonplasticconstructionforaremotesensingoftheearthspaceequipment AT konstantinvmikhaylovskiy developmentofadesignmethodologyforheatloadeddimensionallystableelementsofcarbonplasticconstructionforaremotesensingoftheearthspaceequipment |