@Article{SukhanovPrad:2019:UsTeSw,
author = "Sukhanov, Alexander and Prado, Antonio Fernando Bertachini de
Almeida",
affiliation = "{} and {Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Use of the tethered swingby maneuver to reach the Haumea dwarf
planet",
journal = "Astrophysics and Space Science",
year = "2019",
volume = "364",
number = "1",
month = "jan.",
keywords = "Astrodynamics, Interplanetary misisons, Tethers in space.",
abstract = "The asteroid tethered swingby maneuver (ATSM) is analyzed in this
paper. The maneuver implies turn of the spacecraft velocity by
means of a tether anchored to an asteroid. Mission to Haumea dwarf
planet is considered. The following spacecraft transfer
trajectories with launch in 2025 and 2027 are analyzed in the
paper: Earth-Jupiter-Haumea and Earth-ATSM-Jupiter-Haumea. Only
asteroids bigger than 40km in diameter were considered in order to
make hitting the asteroid by the tether anchor easier. Many Main
Belt asteroids lowering total V of the transfers were found. Afew
of them giving the maximum effect of ATSM were selected and the
transfers using them are analyzed in details. It is shown that the
ATSM using these asteroids would lower substantially the total V
or shorten significantly the time of flight. Technical problems of
the ATSM implementation, such as possibly big mass of the tether
and anchor, difficulty of hitting the asteroid and anchoring the
tether securely etc., are considered. These problems would not
allow to implement the ATSM at present time, but hopefully will be
solved in near future.",
doi = "10.1007/s10509-018-3488-6",
url = "http://dx.doi.org/10.1007/s10509-018-3488-6",
issn = "0004-640X",
language = "en",
targetfile = "sukhanov_use.pdf",
urlaccessdate = "25 abr. 2024"
}