TY - JOUR
T1 - Mission design of DESTINY+
T2 - Toward active asteroid (3200) Phaethon and multiple small bodies
AU - Ozaki, Naoya
AU - Yamamoto, Takayuki
AU - Gonzalez-Franquesa, Ferran
AU - Gutierrez-Ramon, Roger
AU - Pushparaj, Nishanth
AU - Chikazawa, Takuya
AU - Tos, Diogene Alessandro Dei
AU - Çelik, Onur
AU - Marmo, Nicola
AU - Kawakatsu, Yasuhiro
AU - Arai, Tomoko
AU - Nishiyama, Kazutaka
AU - Takashima, Takeshi
PY - 2022
Y1 - 2022
N2 - DESTINY+ is an upcoming JAXA Epsilon medium-class mission to fly by the Geminids meteor shower parent body (3200) Phaethon. It will be the world's first spacecraft to escape from a near-geostationary transfer orbit into deep space using a low-thrust propulsion system. In doing so, DESTINY+ will demonstrate a number of technologies that include a highly efficient ion engine system, lightweight solar array panels, and advanced asteroid flyby observation instruments. These demonstrations will pave the way for JAXA's envisioned low-cost, high-frequency space exploration plans. Following the Phaethon flyby observation, DESTINY+ will visit additional asteroids as its extended mission. The mission design is divided into three phases: a spiral-shaped apogee-raising phase, a multi-lunar-flyby phase to escape Earth, and an interplanetary and asteroids flyby phase. The main challenges include the optimization of the many-revolution low-thrust spiral phase under operational constraints; the design of a multi-lunar-flyby sequence in a multi-body environment; and the design of multiple asteroid flybys connected via Earth gravity assists. This paper shows a novel, practical approach to tackle these complex problems, and presents feasible solutions found within the mass budget and mission constraints. Among them, the baseline solution is shown and discussed in depth; DESTINY+ will spend two years raising its apogee with ion engines, followed by four lunar gravity assists, and a flyby of asteroids (3200) Phaethon and (155140) 2005 UD. Finally, the flight operations plan for the spiral phase and the asteroid flyby phase are presented in detail.
AB - DESTINY+ is an upcoming JAXA Epsilon medium-class mission to fly by the Geminids meteor shower parent body (3200) Phaethon. It will be the world's first spacecraft to escape from a near-geostationary transfer orbit into deep space using a low-thrust propulsion system. In doing so, DESTINY+ will demonstrate a number of technologies that include a highly efficient ion engine system, lightweight solar array panels, and advanced asteroid flyby observation instruments. These demonstrations will pave the way for JAXA's envisioned low-cost, high-frequency space exploration plans. Following the Phaethon flyby observation, DESTINY+ will visit additional asteroids as its extended mission. The mission design is divided into three phases: a spiral-shaped apogee-raising phase, a multi-lunar-flyby phase to escape Earth, and an interplanetary and asteroids flyby phase. The main challenges include the optimization of the many-revolution low-thrust spiral phase under operational constraints; the design of a multi-lunar-flyby sequence in a multi-body environment; and the design of multiple asteroid flybys connected via Earth gravity assists. This paper shows a novel, practical approach to tackle these complex problems, and presents feasible solutions found within the mass budget and mission constraints. Among them, the baseline solution is shown and discussed in depth; DESTINY+ will spend two years raising its apogee with ion engines, followed by four lunar gravity assists, and a flyby of asteroids (3200) Phaethon and (155140) 2005 UD. Finally, the flight operations plan for the spiral phase and the asteroid flyby phase are presented in detail.
KW - (3200) Phaethon
KW - Asteroid flyby
KW - DESTINY
KW - Gravity assist
KW - Low-thrust trajectory
UR - http://www.scopus.com/inward/record.url?scp=85129361215&partnerID=8YFLogxK
U2 - 10.1016/j.actaastro.2022.03.029
DO - 10.1016/j.actaastro.2022.03.029
M3 - Article
AN - SCOPUS:85129361215
SN - 0094-5765
VL - 196
SP - 42
EP - 56
JO - Acta Astronautica
JF - Acta Astronautica
ER -