Main methods of trajectory synthesis for scenarios of space missions with gravity assist maneuvers in the system of Jupiter and with landing on one of its satellites
The development of a methodology for designing trajectories of spacecraft intended for the contact and remote studies of Jupiter and its natural satellites is considered. This methodology should take into account a number of specific features. Firstly, in order to maintain the propellant consumption...
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Veröffentlicht in: | Solar system research 2016-12, Vol.50 (7), p.597-603 |
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creator | Golubev, Yu. F. Tuchin, A. G. Grushevskii, A. V. Koryanov, V. V. Tuchin, D. A. Morskoy, I. M. Simonov, A. V. Dobrovolskii, V. S. |
description | The development of a methodology for designing trajectories of spacecraft intended for the contact and remote studies of Jupiter and its natural satellites is considered. This methodology should take into account a number of specific features. Firstly, in order to maintain the propellant consumption at an acceptable level, the flight profile, ensuring the injection of the spacecraft into orbit around the Jovian moon, should include a large number of gravity assist maneuvers both in the interplanetary phase of the Earth-to-Jupiter flight and during the flight in the system of the giant planet. Secondly, the presence of Jupiter’s powerful radiation belts also imposes fairly strict limitations on the trajectory parameters. |
doi_str_mv | 10.1134/S0038094616070066 |
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subjects | Acceptability Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Gravitation Gravity Jupiter Jupiter (planet) Jupiter satellites Maneuvers Methodology Observations and Techniques Physics Physics and Astronomy Planetology Satellites Space exploration Spacecraft Trajectories |
title | Main methods of trajectory synthesis for scenarios of space missions with gravity assist maneuvers in the system of Jupiter and with landing on one of its satellites |
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