The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements
The paper considers the problem of a small-spacecraft elastic elements’ temperature shock that occurs when the spacecraft immerses into the Earth’s shadow or comes out of it. A small spacecraft with two elastic elements is simulated. In the first approximation, such a problem is considered to be a s...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2023-01-01
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| Series: | Symmetry |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2073-8994/15/1/172 |
| _version_ | 1797436844642664448 |
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| author | Andrey Sedelnikov Denis Orlov Valeria Serdakova Alexandra Nikolaeva |
| author_facet | Andrey Sedelnikov Denis Orlov Valeria Serdakova Alexandra Nikolaeva |
| author_sort | Andrey Sedelnikov |
| collection | DOAJ |
| description | The paper considers the problem of a small-spacecraft elastic elements’ temperature shock that occurs when the spacecraft immerses into the Earth’s shadow or comes out of it. A small spacecraft with two elastic elements is simulated. In the first approximation, such a problem is considered to be a symmetric problem. Estimations of disturbing factors from the temperature shock in a symmetric formulation are obtained. The differences from the results for a small spacecraft with a single elastic element are analyzed. The results of the work can be used for promising small technological spacecraft development, as well as for solving problems of space debris removal and remote sensing of the Earth. |
| first_indexed | 2024-03-09T11:08:28Z |
| format | Article |
| id | doaj.art-c6557f1ea4e54e04ab96e3abf656218c |
| institution | Directory Open Access Journal |
| issn | 2073-8994 |
| language | English |
| last_indexed | 2024-03-09T11:08:28Z |
| publishDate | 2023-01-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Symmetry |
| spelling | doaj.art-c6557f1ea4e54e04ab96e3abf656218c2023-12-01T00:52:58ZengMDPI AGSymmetry2073-89942023-01-0115117210.3390/sym15010172The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic ElementsAndrey Sedelnikov0Denis Orlov1Valeria Serdakova2Alexandra Nikolaeva3Institute of Aerospace Engineering of Samara National Research University, 34 Moskovskoye Shosse, 443086 Samara, RussiaInstitute of Aerospace Engineering of Samara National Research University, 34 Moskovskoye Shosse, 443086 Samara, RussiaInstitute of Aerospace Engineering of Samara National Research University, 34 Moskovskoye Shosse, 443086 Samara, RussiaInstitute of Aerospace Engineering of Samara National Research University, 34 Moskovskoye Shosse, 443086 Samara, RussiaThe paper considers the problem of a small-spacecraft elastic elements’ temperature shock that occurs when the spacecraft immerses into the Earth’s shadow or comes out of it. A small spacecraft with two elastic elements is simulated. In the first approximation, such a problem is considered to be a symmetric problem. Estimations of disturbing factors from the temperature shock in a symmetric formulation are obtained. The differences from the results for a small spacecraft with a single elastic element are analyzed. The results of the work can be used for promising small technological spacecraft development, as well as for solving problems of space debris removal and remote sensing of the Earth.https://www.mdpi.com/2073-8994/15/1/172temperature shocksymmetrical small spacecraftgravity-sensitive technological processesspace tugremote sensing of the Earth |
| spellingShingle | Andrey Sedelnikov Denis Orlov Valeria Serdakova Alexandra Nikolaeva The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements Symmetry temperature shock symmetrical small spacecraft gravity-sensitive technological processes space tug remote sensing of the Earth |
| title | The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements |
| title_full | The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements |
| title_fullStr | The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements |
| title_full_unstemmed | The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements |
| title_short | The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements |
| title_sort | symmetric formulation of the temperature shock problem for a small spacecraft with two elastic elements |
| topic | temperature shock symmetrical small spacecraft gravity-sensitive technological processes space tug remote sensing of the Earth |
| url | https://www.mdpi.com/2073-8994/15/1/172 |
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