Paper
15 April 2008 Deep space flight of Hayabusa asteroid explorer
Hitoshi Kuninaka, Jun'ichiro Kawaguchi
Author Affiliations +
Abstract
The Hayabusa spacecraft rendezvoused with the asteroid Itokawa in 2005 after the powered flight in the deep space by the μ10 cathode-less electron cyclotron resonance ion engines. Though the spacecraft was seriously damaged after the successful soft-landing and lift-off, the xenon cold gas jets from the ion engines rescued it. New attitude stabilization method using a single reaction wheel, the ion beam jets, and the photon pressure was established and enabled the homeward journey from April 2007 aiming the Earth return on 2010. The total accumulated operational time of the ion engines reaches 31,400 hours at the end of 2007. One of four thrusters achieved 13,400-hour space operation.
© (2008) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Hitoshi Kuninaka and Jun'ichiro Kawaguchi "Deep space flight of Hayabusa asteroid explorer", Proc. SPIE 6960, Space Exploration Technologies, 696002 (15 April 2008); https://doi.org/10.1117/12.782163
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CITATIONS
Cited by 4 scholarly publications.
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KEYWORDS
Space operations

Ions

Asteroids

Sun

Xenon

Microwave radiation

Chronology

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