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Plasma energy Angle and Composition Experiment (PACE)
Radio Science (RS)
Upper-atmosphere and Plasma Imager (UPI)
Relay Satellite aboard Okina (RSAT)
VLBI Radio source aboard Okina and Ouna (VRAD)
High Definition Television cameras (HDTV)
SELENE (/ˈsɛlɪniː/; Selenological and Engineering Explorer), better known in Japan by its nickname Kaguya (かぐや), was the second Japanese
lunar orbiter
spacecraft following the
Hiten probe.[4] Produced by the
Institute of Space and Astronautical Science (ISAS) and the
National Space Development Agency (NASDA), the spacecraft was launched on September 14, 2007. After orbiting the Moon for a year and eight months, the main orbiter was instructed to impact on the lunar surface near the crater
Gill on June 10, 2009.[5]
Nickname
The orbiter's nickname, Kaguya, was selected by the general public. It comes from the name of a lunar princess in the ancient
Japanese folktaleThe Tale of the Bamboo Cutter.[6] After their successful release, its sub-satellites, Rstar and Vstar, were named Okina and Ouna, also derived from characters in the tale.[7]
Mission objectives
The main scientific objectives of the mission were to:
SELENE launched on September 14, 2007, at 01:31:01 UTC on an
H-IIA (Model H2A2022) carrier rocket from
Tanegashima Space Center into a 281.55-kilometre (174.95 mi) (
perigee) / 232,960-kilometre (144,750 mi) (
apogee)
geocentricparking orbit.[8][9] The total launch mass was 3,020 kilograms (6,660 lb).[1][2]
The SELENE mission was originally scheduled to launch in 2003, but rocket failures on another mission and technical difficulties delayed the launch until 2007.[10] Launch was planned for August 16, 2007, but was postponed when some electronic components were found to be installed incorrectly.[11]
Lunar operations
On October 3, it entered an initial 101-to-11,741-kilometre (63 to 7,296 mi) polar lunar orbit.[12]
On October 9, the relay satellite was released into a 100-to-2,400-kilometre (62 to 1,491 mi) orbit, while on October 12 the VLBI satellite was released into a 100-to-800-kilometre (62 to 497 mi) one.[7] Finally, by October 19, the orbiter was in a circular 100-kilometre (62 mi) orbit.[13] The nominal mission duration was one year plus possible extensions.
On October 31, 2007, Kaguya deployed its Lunar Magnetometer, Lunar Radar Sounder, Earth-looking Upper Atmosphere and Plasma Imager. On December 21, 2007, Kaguya began regular operations after all fifteen observation experiments had been satisfactorily verified.
Kaguya completed the planned operation by the end of October 2008 and began extended operations planned to continue through March 2009. It would then be sent into a circular 50-kilometre (31 mi) orbit, and finally to an elliptical 20-to-100-kilometre (12 to 62 mi) one, with a controlled impact occurring by August 2009.[14] Because of a degraded
reaction wheel, the plan was changed so that on February 1, 2009, the orbit was lowered to 50 kilometres (31 mi) ± 20 kilometres (12 mi),[15]
and impact with lunar surface occurred at 18:25 UTC on June 10, 2009.[5]
Okina (formerly Rstar) and Ouna (formerly Vstar) were octagonal prisms to support radio science. Okina
relayed radio communications between the orbiter and the Earth when the orbiter was behind the Moon. This allowed, for the first time, the direct
Doppler shift measurements needed
to precisely map the gravitational field of the lunar farside; previously, the farside gravity field could only be inferred by nearside measurements. The relay satellite impacted the lunar farside near the
Mineur D crater at 19:46 JST (10:46 UTC) on February 12, 2009.[15]
Function: two-way radio science relay, orbiter-earth
Initial orbit: 100 to 2,400 kilometres (62 to 1,491 mi)
Inclination: 90 degrees
Ouna (VLBI satellite)
Ouna used
Very Long Baseline Interferometry as a second way to map the Moon's gravity field. It was especially useful at the
lunar limb, where the gravitational acceleration is perpendicular to the line of sight to Earth, making Doppler measurements unsuitable.
Function: VLBI radio science
Mass: 53 kilograms (117 lb)
Size: 1.0 x 1.0 x 0.65 m (3.3 x 3.3 x 2.1 ft)
Attitude control: spin-stabilized
Power: 70 W
Initial orbit: 100 to 800 kilometres (62 to 497 mi)
Inclination: 90 degrees
Instruments
SELENE carried 13 scientific instruments "to obtain scientific data of the lunar origin and evolution and to develop the technology for the future lunar exploration":[17]
Terrain camera (TC) (resolution 10 meters [33 ft] per pixel)[18]
Radio wave source for VLBI (VRAD) aboard Okina and Ouna
Two 2.2 megapixel CCD
HDTVcameras, one wide-angle and one telephoto, were also on board, primarily for public outreach.[19] The HDTV system, developed by
NHK (Japan Broadcasting Corporation), produced over 1.3 TB of video and stills over 19 months.[20]
JAXA collected names and messages that were carried on SELENE through their "Wish Upon the Moon" campaign.[21] 412,627 names and messages were printed on a sheet measuring 280 mm x 160 mm (11 x 6.3 in) at 70
µm (0.0003 in) per character. The sheet was installed under the
photovoltaic modules and cooling panels beneath the multi-layered insulation.[22]
Results
Major results include:
Improved lunar global topography maps.[23] This detailed altitude and geological data was provided to Google for free to make Google Moon 3-D.
First optical observation of the permanently shadowed interior of the crater
Shackleton at the lunar south pole.[25]
Evidence of Earth's oxygen being transported to the Moon via
magnetospheric ions.[26]
Other lunar probes
SELENE was part of a renewed global interest in lunar exploration; it was "the largest lunar mission since the
Apollo program".[27] It followed Japan's first lunar probe,
Hagoromo, launched in 1990.[4][28] China launched its
Chang'e 1 lunar explorer on October 24, 2007, followed by India's October 22, 2008 launch of
Chandrayaan-1 and the United States
Lunar Reconnaissance Orbiter in June 2009. The United States, European countries (
ESA), Russia, Japan, India and China are planning
future crewed lunar exploration missions or
lunar outpost construction on the Moon between 2018 and 2025.[29]
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).