The Proceedings of the Space Engineering Conference
Online ISSN : 2424-3191
ISSN-L : 0918-9238
2002.10
Session ID : A4
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A4 R&D of Small Satellites : Research scenario on 50kg class micro satellites
Hidekazu HASHIMOTO
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CONFERENCE PROCEEDINGS FREE ACCESS

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Abstract
The mainstream of the research and development of satellites in NASDA is for over 1 ton-class satellite. But, 50kg-class Micro satellites and under 10kg-class Nano satellites are researched, too. "μ-Lab Sat" -the first Micro satellite in NASDA- is planning to launch in 2002. The orbit of this satellite is LEO (low earth orbit) and the attitude of this satellite is the spin stabilization mainly, and the three-axis stabilization in the experiment. "μ-Lab Sat 2"-the next micro satellite in NASDA, is under conceptual study. It has 30kg-class mother ship satellite and 5〜10kg-class daughter-ship satellites. The orbit of this satellite is GTO (geostationary transfer orbit) and the attitude of mother ship satellite is the three-axis stabilization. Daughter-ship satellites will be formation flying in the experiment. The formation flying is the key technique for the interferometer.
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© 2002 The Japan Society of Mechanical Engineers
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