Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface
The article presents the results of a study on the basis of which a set of mathematical models was developed for ballistic analysis of a mission to send a small spacecraft to the satellite of Jupiter, Callisto and its landing on the surface of the satellite. In this mission, it is proposed to use a...
| الحاوية / القاعدة: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
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| المؤلفون الرئيسيون: | , , , |
| التنسيق: | مقال |
| اللغة: | الإنجليزية |
| منشور في: |
Samara National Research University
2024-04-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://journals.ssau.ru/vestnik/article/viewFile/27326/10460 |
| _version_ | 1850373606253527040 |
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| author | V. V. Kovalev A. D. Marchenko T. V. Starostina A. R. Sharipova |
| author_facet | V. V. Kovalev A. D. Marchenko T. V. Starostina A. R. Sharipova |
| author_sort | V. V. Kovalev |
| collection | DOAJ |
| container_title | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
| description | The article presents the results of a study on the basis of which a set of mathematical models was developed for ballistic analysis of a mission to send a small spacecraft to the satellite of Jupiter, Callisto and its landing on the surface of the satellite. In this mission, it is proposed to use a gravity assist maneuver around the Earth and an aerodynamic maneuver near Jupiter to reduce the cost of the working fluid of the spacecraft. The minimum required thrust of the engines and the duration of the soft landing maneuver of a spacecraft with a given mass on the satellite are estimated. The optimal launch date was found for the possibility of launching a spacecraft using a medium-lift Soyuz-2 launch vehicle. The simulation of the movement was carried out numerically, in the Mathcad mathematical package, all the dependence diagrams necessary for the analysis of the movement were constructed. |
| format | Article |
| id | doaj-art-0b16f10f4fa14fbeaf151fc2ac96b31e |
| institution | Directory of Open Access Journals |
| issn | 2542-0453 2541-7533 |
| language | English |
| publishDate | 2024-04-01 |
| publisher | Samara National Research University |
| record_format | Article |
| spelling | doaj-art-0b16f10f4fa14fbeaf151fc2ac96b31e2025-08-19T23:00:19ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332024-04-01231213710.18287/2541-7533-2024-23-1-21-378886Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surfaceV. V. Kovalev0A. D. Marchenko1T. V. Starostina2A. R. Sharipova3Samara National Research UniversitySamara National Research UniversitySamara National Research UniversitySamara National Research UniversityThe article presents the results of a study on the basis of which a set of mathematical models was developed for ballistic analysis of a mission to send a small spacecraft to the satellite of Jupiter, Callisto and its landing on the surface of the satellite. In this mission, it is proposed to use a gravity assist maneuver around the Earth and an aerodynamic maneuver near Jupiter to reduce the cost of the working fluid of the spacecraft. The minimum required thrust of the engines and the duration of the soft landing maneuver of a spacecraft with a given mass on the satellite are estimated. The optimal launch date was found for the possibility of launching a spacecraft using a medium-lift Soyuz-2 launch vehicle. The simulation of the movement was carried out numerically, in the Mathcad mathematical package, all the dependence diagrams necessary for the analysis of the movement were constructed.https://journals.ssau.ru/vestnik/article/viewFile/27326/10460spacecraftinterplanetary flightgravity assistmathematical modelingpiecewise conical approximationjupiter’s moon callistolanding on the surface |
| spellingShingle | V. V. Kovalev A. D. Marchenko T. V. Starostina A. R. Sharipova Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface spacecraft interplanetary flight gravity assist mathematical modeling piecewise conical approximation jupiter’s moon callisto landing on the surface |
| title | Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface |
| title_full | Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface |
| title_fullStr | Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface |
| title_full_unstemmed | Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface |
| title_short | Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface |
| title_sort | ballistic analysis of a mission to jupiter s moon callisto with landing on the surface |
| topic | spacecraft interplanetary flight gravity assist mathematical modeling piecewise conical approximation jupiter’s moon callisto landing on the surface |
| url | https://journals.ssau.ru/vestnik/article/viewFile/27326/10460 |
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