This page is on the proposed lunar spacecraft. For the Greek goddess, see Selene

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SELENE is a proposed Japanese lunar orbiter spacecraft. The name stands for SELenological and ENgineering Explorer, and it is produced by ISAS for NASDA. The proposed launch period is in September - December 2005.

There are three separate units comprising the spacecraft. The main orbiter is a rectangular box measuring about 2.1 m by 4.2 m, with a mass of about 1600 kg. A small relay satellite and a VLBI satellite are both octagonal prisms. The relay satellite transmits communications from the orbiter to Earth, and the VLBI satellite will be used to measure the position and precession of the moon precisely.

Included in the 13 instruments carries are imagers, a radar sounder, a laser altimeter, an X-ray fluorescence spectrometer and a gamma-ray spectrometer. The goal is to study the origin, evolution and tectonics of the Moon from orbit.

The total launch mass will be 2000 kg, and it will be launched from the Tanegashima Space Center by an H-2A rocket. Five days later, it will reach the moon and enter an initial 120 x 13000 km polar orbit. The relay satellite will move to a 100 x 2400 km orbit, and the VLBI satellite will move to a 100 x 800 km orbit. Finally, the orbiter will move to a 100 km circular orbit. The expected life of the mission is one year.

External links

• NASDA site http://moon.nasda.go.jp/en/selene/index.html