Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface
- Authors: Kovalev V.V.1, Marchenko A.D.1, Starostina T.V.1, Sharipova A.R.1
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Affiliations:
- Samara National Research University
- Issue: Vol 23, No 1 (2024)
- Pages: 21-37
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.rcsi.science/2542-0453/article/view/311444
- DOI: https://doi.org/10.18287/2541-7533-2024-23-1-21-37
- ID: 311444
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Abstract
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.
About the authors
V. V. Kovalev
Samara National Research University
Author for correspondence.
Email: vadkovalev97@mail.ru
Postgraduate Student of the Department of Flight Dynamics and Control Systems
Russian FederationA. D. Marchenko
Samara National Research University
Email: anzhela_marchenko_97@mail.ru
Postgraduate Student of the Department of Flight Dynamics and Control Systems
Russian FederationT. V. Starostina
Samara National Research University
Email: samara-tanya2000@mail.ru
Student of the Institute of Aeronautical and Space Rocket Engineering
Russian FederationA. R. Sharipova
Samara National Research University
Email: Sharipovaaliya2016@yandex.ru
Postgraduate Student of the Department of Flight Dynamics and Control Systems
Russian FederationReferences
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