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SELENE

SELENE (/ˈsɛlɪn/; 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 successfully 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]

Kaguya
Mission typeLunar orbiter
OperatorJAXA
COSPAR ID2007-039A
SATCAT no.32054
Mission duration1 year and 9 months (launch date to decay date)
Spacecraft properties
ManufacturerNEC Toshiba Space Systems
Launch massTotal: 3,020 kilograms (6,660 lb)
* Main orbiter (Kaguya): 2,914 kilograms (6,424 lb)
* Relay Satellite (Okina): 53 kilograms (117 lb)
* VLBI Satellite (Ouna): 53 kilograms (117 lb)[1][2]
Power3,486 watts
Start of mission
Launch dateSeptember 14, 2007, 01:31:01 (2007-09-14UTC01:31:01Z) UTC
RocketH-IIA 2022 F13
Launch siteTanegashima Yoshinobu 1
ContractorMitsubishi
End of mission
Decay dateJune 10, 2009, 18:25 (2009-06-10UTC18:26Z) UTC
Orbital parameters
Reference systemSelenocentric
Periselene altitude281 kilometres (175 mi)[3]
Aposelene altitude231,910 kilometres (144,100 mi)[3]
Inclination29.9 degrees[3]
Period7109.28 seconds[3]
EpochSeptember 29, 2007[3]
Lunar orbiter
Orbital insertionOctober 3, 2007
Instruments
  • X-ray Spectrometer (XRS)
  • gamma-ray spectrometer (GRS)
  • Multi-band Imager (MI)
  • Spectral Profiler (SP)
  • Terrain Camera (TC)
  • Lunar Radar Sounder (LRS)
  • Laser Altimeter (LALT)
  • Lunar Magnetometer (LMAG)
  • Charged Particle Spectrometer (CPS)
  • 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)
 

Nickname Edit

The orbiter's nickname, Kaguya, was selected by the general public. It comes from the name of a lunar princess in the ancient Japanese folktale The 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 Edit

The main scientific objectives of the mission were to:

Launch Edit

 
Launch of H-IIA F13 carrying SELENE (Photo by Narita Masahiro)

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) geocentric parking 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 Edit

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]

Design Edit

The mission featured three separate spacecraft:

Main orbiter[1] Edit

Okina (small relay satellite) Edit

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
  • Mass: 53 kilograms (117 lb)[1]
  • 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 2,400 kilometres (62 to 1,491 mi)
  • Inclination: 90 degrees

Ouna (VLBI satellite) Edit

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 Edit

 
First optical still captured by the onboard HDTV camera. Earth is seen at a distance of 11,000 km.[16]

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]
  • X-ray fluorescence spectrometer (XRS)
  • Lunar magnetometer (LMAG)
  • Spectral profiler (SP) (resolution per pixel: 562 x 400 m [1840 x 1310 ft)
  • Multi-band imager (MI) (resolution of visible light 20 [66 ft] meters per pixel, near-infrared 62 meters [200 ft] per pixel)
  • Laser altimeter (LALT)
  • Lunar radar sounder (LRS)
  • Gamma ray spectrometer (GRS)
  • Charged particle spectrometer (CPS)
  • Plasma analyzer (PACE)
  • Upper atmosphere and plasma imager (UPI)
  • Radio wave repeater (RSAT) aboard Okina
  • Radio wave source for VLBI (VRAD) aboard Okina and Ouna

Two 2.2 megapixel CCD HDTV cameras, 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 Edit

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.
  • Detailed gravity map of the far side of the Moon.[24]
  • 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 Edit

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]

See also Edit

References Edit

  1. ^ a b c d "平成19年度夏期ロケット打ち上げおよび追跡管制計画書 (Rocket Launch and Tracking Control Plan, Summer 2007)" (PDF) (in Japanese). MHI / JAXA.
  2. ^ a b "SELENE/Kaguya" (PDF). NASA. Retrieved 2022-12-02.
  3. ^ a b c d e McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 2018-05-03.
  4. ^ a b . Red Orbit. 2007-09-14. Archived from the original on 2011-05-22. Retrieved 2007-09-14.
  5. ^ a b "KAGUYA Lunar Impact". JAXA. Retrieved 2009-06-24.
  6. ^ ""KAGUYA" selected as SELENE's nickname". Retrieved 2007-10-13.
  7. ^ a b (Press release). 2007-10-12. Archived from the original on 2012-03-20. Retrieved 2007-10-13.
  8. ^ Emily Lakdawalla (2007-09-14). . Archived from the original on 2012-02-06. Retrieved 2007-09-15.
  9. ^ MHI / JAXA. "H-IIAロケット13号機による月周回衛星「かぐや」の打上げ結果について(速報)" (PDF) (in Japanese). Retrieved 2007-09-19.
  10. ^ "Japan launches first lunar probe". BBC News. 2007-09-14. Retrieved 2007-09-14.
  11. ^ "Launch Postponement of the KAGUYA (SELENE)". 2007-07-20. Retrieved 2007-08-15.
  12. ^ (Press release). JAXA. 2007-10-05. Archived from the original on 2012-05-14. Retrieved 2007-10-05.
  13. ^ "かぐや/H-IIA13号機 打上げ特設サイト" (in Japanese). Retrieved 2007-10-01.
  14. ^ "月周回衛星「かぐや(SELENE)」の定常運用終了と後期運用計画について" (PDF) (in Japanese). 2008-11-05. Retrieved 2008-11-05.
  15. ^ a b "月周回衛星「かぐや(SELENE)」の 状況について" (PDF) (in Japanese). 2009-02-18. Retrieved 2009-02-22.
  16. ^ "PDAP Search Results".
  17. ^ "Kaguya (SELENE)". JAXA. Retrieved 2007-06-25.
  18. ^ "LISM [TC, MI, SP]". Kaguya (SELENE). JAXA. Retrieved 2007-06-25.
  19. ^ "KAGUYA (SELENE) – Mission Instruments – HDTV". Retrieved 2009-03-01.
  20. ^ "Results of High-Definition Television System (HDTV) on Board SELENE (KAGUYA)" (PDF). 40th Lunar and Planetary Science Conference (2009). Retrieved 2022-12-09.
  21. ^ (Press release). The Planetary Society. 2007-01-11. Archived from the original on 2012-02-12. Retrieved 2007-07-14.
  22. ^ (in Japanese). JAXA. 2007. Archived from the original on 2007-04-04. Retrieved 2007-07-14.
  23. ^ H. Araki; et al. (2009-02-13). "Lunar Global Shape and Polar Topography Derived from Kaguya-LALT Laser Altimetry". Science. 323 (5916): 897–900. Bibcode:2009Sci...323..897A. doi:10.1126/science.1164146. PMID 19213910. S2CID 2115707.
  24. ^ N. Namiki; et al. (2009-02-13). "Farside Gravity Field of the Moon from Four-Way Doppler Measurements of SELENE (Kaguya)". Science. 323 (5916): 900–905. Bibcode:2009Sci...323..900N. doi:10.1126/science.1168029. PMID 19213911. S2CID 5306227.
  25. ^ J. Haruyama; et al. (2008-11-07). "Lack of Exposed Ice Inside Lunar South Pole Shackleton Crater". Science. 322 (5903): 938–939. Bibcode:2008Sci...322..938H. doi:10.1126/science.1164020. PMID 18948501. S2CID 20749838.
  26. ^ Terada, Kentaro; Yokota, Shoichiro; Saito, Yoshifumi; Kitamura, Naritoshi; Asamura, Kazushi; Nishino, Masaki (2017-01-30). "Biogenic oxygen from Earth transported to the Moon by a wind of magnetospheric ions". Nature Astronomy. 1 (2): 0026. Bibcode:2017NatAs...1E..26T. doi:10.1038/s41550-016-0026. S2CID 85560607.
  27. ^ . Archived from the original on 2013-10-24. Retrieved 2008-04-21.
  28. ^ "Hiten". NASA. Retrieved 2007-09-14.
  29. ^ . Library of Congress. 2008-10-22. Archived from the original on 2016-07-04. Retrieved 2008-10-22.

External links Edit

  • (in English) Official project site, JAXA
  • (in English) Official launch information site, JAXA
  • by NASA's Solar System Exploration
  • (in English) , ISAS/JAXA
  • (in English) Official YouTube channel, JAXA
  • (in English) June 10th impact location 2013-07-18 at the Wayback Machine
  • (in English) , NEC Corporation
  • – Video 12 min. before impact – close surface flyover

selene, second, series, lunar, spacecraft, other, uses, selene, disambiguation, help, expand, this, article, with, text, translated, from, corresponding, article, japanese, december, 2018, click, show, important, translation, instructions, view, machine, trans. For the second SELENE series lunar spacecraft see SELENE 2 For other uses see Selene disambiguation You can help expand this article with text translated from the corresponding article in Japanese December 2018 Click show for important translation instructions View a machine translated version of the Japanese article Machine translation like DeepL or Google Translate is a useful starting point for translations but translators must revise errors as necessary and confirm that the translation is accurate rather than simply copy pasting machine translated text into the English Wikipedia Consider adding a topic to this template there are already 3 556 articles in the main category and specifying topic will aid in categorization Do not translate text that appears unreliable or low quality If possible verify the text with references provided in the foreign language article You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation A model attribution edit summary is Content in this edit is translated from the existing Japanese Wikipedia article at ja かぐや see its history for attribution You should also add the template Translated ja かぐや to the talk page For more guidance see Wikipedia Translation SELENE ˈ s ɛ l ɪ n iː 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 successfully 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 KaguyaMission typeLunar orbiterOperatorJAXACOSPAR ID2007 039ASATCAT no 32054Mission duration1 year and 9 months launch date to decay date Spacecraft propertiesManufacturerNEC Toshiba Space SystemsLaunch massTotal 3 020 kilograms 6 660 lb Main orbiter Kaguya 2 914 kilograms 6 424 lb Relay Satellite Okina 53 kilograms 117 lb VLBI Satellite Ouna 53 kilograms 117 lb 1 2 Power3 486 wattsStart of missionLaunch dateSeptember 14 2007 01 31 01 2007 09 14UTC01 31 01Z UTCRocketH IIA 2022 F13Launch siteTanegashima Yoshinobu 1ContractorMitsubishiEnd of missionDecay dateJune 10 2009 18 25 2009 06 10UTC18 26Z UTCOrbital parametersReference systemSelenocentricPeriselene altitude281 kilometres 175 mi 3 Aposelene altitude231 910 kilometres 144 100 mi 3 Inclination29 9 degrees 3 Period7109 28 seconds 3 EpochSeptember 29 2007 3 Lunar orbiterOrbital insertionOctober 3 2007InstrumentsX ray Spectrometer XRS gamma ray spectrometer GRS Multi band Imager MI Spectral Profiler SP Terrain Camera TC Lunar Radar Sounder LRS Laser Altimeter LALT Lunar Magnetometer LMAG Charged Particle Spectrometer CPS 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 Contents 1 Nickname 2 Mission objectives 3 Launch 4 Lunar operations 5 Design 5 1 Main orbiter 1 5 2 Okina small relay satellite 5 3 Ouna VLBI satellite 6 Instruments 7 Results 8 Other lunar probes 9 See also 10 References 11 External linksNickname EditThe orbiter s nickname Kaguya was selected by the general public It comes from the name of a lunar princess in the ancient Japanese folktale The 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 EditThe main scientific objectives of the mission were to Study the origins of the Moon and its geologic evolution Obtain information about the lunar surface environment Perform radio science especially precise measurement of the Moon s gravity fieldLaunch Edit nbsp Launch of H IIA F13 carrying SELENE Photo by Narita Masahiro 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 geocentric parking 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 EditOn 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 Design EditThe mission featured three separate spacecraft Main orbiter 1 Edit Shape octagonal prism Mass 2 914 kilograms 6 424 lb Size 2 1 x 2 1 x 4 8 m 6 9 x 6 9 x 16 ft Attitude control Three axis stabilized Power 3 5 kW Max Mission period 1 year Mission orbit Circular 100 kilometre 62 mi Inclination 90 degreesOkina small relay satellite Edit 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 Mass 53 kilograms 117 lb 1 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 2 400 kilometres 62 to 1 491 mi Inclination 90 degreesOuna VLBI satellite Edit 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 degreesInstruments Edit nbsp First optical still captured by the onboard HDTV camera Earth is seen at a distance of 11 000 km 16 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 X ray fluorescence spectrometer XRS Lunar magnetometer LMAG Spectral profiler SP resolution per pixel 562 x 400 m 1840 x 1310 ft Multi band imager MI resolution of visible light 20 66 ft meters per pixel near infrared 62 meters 200 ft per pixel Laser altimeter LALT Lunar radar sounder LRS Gamma ray spectrometer GRS Charged particle spectrometer CPS Plasma analyzer PACE Upper atmosphere and plasma imager UPI Radio wave repeater RSAT aboard Okina Radio wave source for VLBI VRAD aboard Okina and OunaTwo 2 2 megapixel CCD HDTV cameras 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 EditMajor 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 Detailed gravity map of the far side of the Moon 24 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 EditSELENE 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 See also Edit nbsp Spaceflight portalSELENE 2 List of missions to the Moon Exploration of the MoonReferences Edit a b c d 平成19年度夏期ロケット打ち上げおよび追跡管制計画書 Rocket Launch and Tracking Control Plan Summer 2007 PDF in Japanese MHI JAXA a b SELENE Kaguya PDF NASA Retrieved 2022 12 02 a b c d e McDowell Jonathan Satellite Catalog Jonathan s Space Page Retrieved 2018 05 03 a b Kaguya Another Chapter for the Lunar Saga Red Orbit 2007 09 14 Archived from the original on 2011 05 22 Retrieved 2007 09 14 a b KAGUYA Lunar Impact JAXA Retrieved 2009 06 24 KAGUYA selected as SELENE s nickname Retrieved 2007 10 13 a b KAGUYA SELENE Result of the Separation of the VRAD Satellite Vstar Press release 2007 10 12 Archived from the original on 2012 03 20 Retrieved 2007 10 13 Emily Lakdawalla 2007 09 14 Kaguya Rockets Toward the Moon Archived from the original on 2012 02 06 Retrieved 2007 09 15 MHI JAXA H IIAロケット13号機による月周回衛星 かぐや の打上げ結果について 速報 PDF in Japanese Retrieved 2007 09 19 Japan launches first lunar probe BBC News 2007 09 14 Retrieved 2007 09 14 Launch Postponement of the KAGUYA SELENE 2007 07 20 Retrieved 2007 08 15 KAGUYA SELENE Result of the Lunar Orbit Injection Maneuver LOI1 Lunar orbit injection was confirmed Press release JAXA 2007 10 05 Archived from the original on 2012 05 14 Retrieved 2007 10 05 かぐや H IIA13号機 打上げ特設サイト in Japanese Retrieved 2007 10 01 月周回衛星 かぐや SELENE の定常運用終了と後期運用計画について PDF in Japanese 2008 11 05 Retrieved 2008 11 05 a b 月周回衛星 かぐや SELENE の 状況について PDF in Japanese 2009 02 18 Retrieved 2009 02 22 PDAP Search Results Kaguya SELENE JAXA Retrieved 2007 06 25 LISM TC MI SP Kaguya SELENE JAXA Retrieved 2007 06 25 KAGUYA SELENE Mission Instruments HDTV Retrieved 2009 03 01 Results of High Definition Television System HDTV on Board SELENE KAGUYA PDF 40th Lunar and Planetary Science Conference 2009 Retrieved 2022 12 09 Send a New Year s Message to the Moon on Japan s SELENE Mission Buzz Aldrin Ray Bradbury and More Have Wished Upon the Moon Press release The Planetary Society 2007 01 11 Archived from the original on 2012 02 12 Retrieved 2007 07 14 セレーネ 月に願いを SELENE Wish Upon the Moon in Japanese JAXA 2007 Archived from the original on 2007 04 04 Retrieved 2007 07 14 H Araki et al 2009 02 13 Lunar Global Shape and Polar Topography Derived from Kaguya LALT Laser Altimetry Science 323 5916 897 900 Bibcode 2009Sci 323 897A doi 10 1126 science 1164146 PMID 19213910 S2CID 2115707 N Namiki et al 2009 02 13 Farside Gravity Field of the Moon from Four Way Doppler Measurements of SELENE Kaguya Science 323 5916 900 905 Bibcode 2009Sci 323 900N doi 10 1126 science 1168029 PMID 19213911 S2CID 5306227 J Haruyama et al 2008 11 07 Lack of Exposed Ice Inside Lunar South Pole Shackleton Crater Science 322 5903 938 939 Bibcode 2008Sci 322 938H doi 10 1126 science 1164020 PMID 18948501 S2CID 20749838 Terada Kentaro Yokota Shoichiro Saito Yoshifumi Kitamura Naritoshi Asamura Kazushi Nishino Masaki 2017 01 30 Biogenic oxygen from Earth transported to the Moon by a wind of magnetospheric ions Nature Astronomy 1 2 0026 Bibcode 2017NatAs 1E 26T doi 10 1038 s41550 016 0026 S2CID 85560607 SELENE The largest lunar mission since the Apollo program Archived from the original on 2013 10 24 Retrieved 2008 04 21 Hiten NASA Retrieved 2007 09 14 NASA Authorization Act of 2008 Section 404 Lunar Outpost Library of Congress 2008 10 22 Archived from the original on 2016 07 04 Retrieved 2008 10 22 External links Edit nbsp Wikinews has related news Japan s lunar probe performing smoothly after successful launch in English Official project site JAXA in English Official launch information site JAXA SELENE Mission Profile by NASA s Solar System Exploration in English SELENE overview ISAS JAXA in English Official YouTube channel JAXA in English June 10th impact location Archived 2013 07 18 at the Wayback Machine in English NEC Corporation s Kaguya page NEC Corporation JAXA Link Video 12 min before impact close surface flyover Retrieved from https en wikipedia org w index php title SELENE amp oldid 1179234721, wikipedia, wiki, book, books, library,

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