The Proceedings of the Space Engineering Conference
Online ISSN : 2424-3191
ISSN-L : 0918-9238
2010.19
Session ID : D4
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D4 Outline and Results of In-flight Operation of a CubeSat HAYATO(KSAT)
Masanori NishioHiroshi KatanodaRyota HayashiYuji SakamotoYuji HaradaShinichi Teshima
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CONFERENCE PROCEEDINGS FREE ACCESS

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Abstract

A pico-satellite HAYATO (KSAT) was launched on the piggyback of HIIA 17 from Tanegashima Space Center on May 21, 2010, and put into a circular orbit of altitude of 300 km. HAYATO has a 10-cm cube structure and is the first CubeSat onboard a Ku-band transmitter. We had successfully caught telemetry signals with a ground control system at Kagoshima University after eleven days of the satellite launch. Despite of a limited operation period, we have confirmed that most of bus components, such as solar cells, a power control unit, secondary batteries, and onboard computer and a Ku-band transmitter, were survived space environment during eighteen days.

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© 2011 The Japan Society of Mechanical Engineers
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