Kazutaka Nishiyama, Satoshi Hosoda, Ryudo Tsukizaki, Hitoshi Kuninaka
Proceedings of the International Astronautical Congress, IAC, 2018-October, 2018 Lead author
Copyright © 2018 by the International Astronautical Federation (IAF). All rights reserved. Japan's second asteroid explorer Hayabusa2 was successfully launched on Dec 3, 2014 for sample return from Asteroid 162173 Ryugu by 2020. Four xenon ion thrusters using electron cyclotron resonance discharge propelled the spacecraft for 547 hours during the first year in space. Hayabusa2 completed an Earth gravity assist on Dec 3, 2015 followed by 798 hours and 2,593 hours of ion thruster operations called the first- and second- term transfer delta-V. The spacecraft has completed the third-term transfer delta-v period between January 10, 2018 and June 6, 2018 in which the final 2,475-hour ion thruster operation was executed before the rendezvous with Ryugu. Cumulative operating hours for four ion thrusters are 6,450 h, 11 h, 5,193 h and 6,418 h, respectively. This paper summarizes the 6,515-hour powered flight by the ion engine system producing 1,015 m/s delta-v, thruster performance change trend, roll torques generated during different combinations of ion thrusters operated, and spacecraft surface erosion histories measured by two quartz crystal microbalances located in the vicinity of the thrusters. In parallel to the space flight operation, an engineering model of microwave discharge neutralizer has been under long-duration testing on the ground since 2012 and accumulated 51,000 hours of diode-mode operation as of September 17, 2018.