Abstract
This study is devoted to the features of designing the flight trajectories to the Solar System center for two promising Russian spacecraft. The scientific goal of this project is studying the circumsolar space from close distances (60–80 solar radii) and extraecliptic inclinations. The planes of the spacecraft operational orbits should be inclined in opposite directions with respect to the Sun’s rotation axis. The description of the spacecraft trajectories and the main characteristics of their flight profiles are presented.
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REFERENCES
Asyushkin, V.A., Vikulenkov, V.P., and Ishin, S.V., Outcome of development and initial operational phases of versatile space tugs of the Fregat type, Sol. Syst. Res., 2015, vol. 49, no. 7, pp. 460–466.
Asyushkin, V.A., Vikulenkov, V.P., Ishin, S.V., Fedoskin, D.I., et al., Enhanced power-capacity multi-purpose versatile tug FREGAT-CBU, Vestn. NPO im. S.A. Lavochkina, 2017, no. 2, pp. 147–156.
Kuznetsov, V.D., Space studies at the Pushkov Institute of Terrestrial Magnetism, Ionosphere and Radio Wave Propagation, Russian Academy of Sciences, in Elektromagnitnye i plazmennye protsessy ot nedr Solntsa do nedr Zemli (Electromagnetic and Plasma Processes from the Bowels of Sun until the Bowels of Earth), Kuznetsov, V.D., Ed., Moscow: Inst. Zemnogo Magn., Ionosfery Raspr. Radiovoln im. N.V. Pushkova, Ross. Akad. Nauk, 2015, pp. 347–368.
Kuznetsov, V.D., Andreevskyi, S.E., Dokukin, V.S., Fomichev, V.V., et al., The Sun and heliosphere explorer—the Interhelioprobe mission, Geomagn. Aeronomy, 2016, vol. 56, no. 7, pp. 781–841.
Malyshev, V.V., Pichkhadze, K.M., and Usachev, E.V., Sistemnyi analiz variantov missii i sintez programmy pryamykh issledovanii blizhaishego okolosolnechnogo prostranstva (System Analysis of Mission Variants and the Way to Synthesize the Program for Direct Investigations of the Nearest Solar Space), Moscow: Mosk. Aviats. Inst., 2006.
Platov, I.V., Simonov, A.V., and Konstantinov, M.S., Choosing an efficient option of the combined propulsion system and flight profile of the INTERHELIO-PROBE spacecraft, Sol. Syst. Res., 2016, vol. 50, no. 7, pp. 581–586.
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Platov, I.V., Simonov, A.V. Design of a Rational Mission Profile for the Flight of Spacecraft to the Solar System Center. Sol Syst Res 53, 593–598 (2019). https://doi.org/10.1134/S0038094619070190
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DOI: https://doi.org/10.1134/S0038094619070190