Jump to content

IKAROS

From Wikipedia, the free encyclopedia

IKAROS
IKAROS model
A 1:64 scale model of the 14 m × 14 m (46 ft × 46 ft) sized IKAROS spacecraft
Mission typeSolar sail technology
OperatorJAXA[1][2][3][4]
COSPAR ID2010-020E Edit this at Wikidata
SATCAT no.36577
Websiteglobal.jaxa.jp/projects/sas/ikaros/
Mission duration5 years launch to last contact in 2015
Spacecraft properties
Launch mass310 kg[5]
DimensionsSolar sail: 14 m × 14 m (46 ft × 46 ft) (area: 196 m2 (2,110 sq ft))[6]
Start of mission
Launch date21:58:22, 20 May 2010 (UTC) (2010-05-20T21:58:22Z)
RocketH-IIA 202
Launch siteTanegashima, LA-Y
End of mission
Last contact20 May 2015[7]
Orbital parameters
Reference systemHeliocentric orbit
Flyby of Venus
Closest approach8 December 2010
Distance80,800 kilometers (50,200 mi)

IKAROS (Interplanetary Kite-craft Accelerated by Radiation Of the Sun) is a Japan Aerospace Exploration Agency (JAXA) experimental spacecraft. The spacecraft was launched on 20 May 2010, aboard an H-IIA rocket, together with the Akatsuki (Venus Climate Orbiter) probe and four other small spacecraft. IKAROS is the first spacecraft to successfully demonstrate solar sail technology in interplanetary space.[3][8] The craft's name is an allusion to the legendary Icarus (Ancient Greek: Ἴκαρος, Ikaros), who flew close to the Sun on wings made of bird-feathers and wax.[9]

On 8 December 2010, IKAROS flew by Venus at a distance of 80,800 km (50,200 mi), successfully completing its planned mission, and entered its extended operation phase.[10][11][12][13]

Purpose

[edit]

The IKAROS probe is the world's first spacecraft to use solar sailing as the main propulsion.[14] It was designed to demonstrate four key technologies (comments in parentheses refer to figure):

  1. Deployment and control of a large, thin solar sail membrane (grey-blue areas numbered 3)
  2. Thin-film solar cells integrated into the sail to power the payload (black rectangles numbered 4)
  3. Measurement of acceleration due to radiation pressure on the solar sail
  4. Attitude control by varying the reflectance of 80 liquid crystal panels embedded in the sail (orange rectangles numbered 2)

The mission also includes investigations of aspects of interplanetary space, such as gamma-ray bursts, solar wind and cosmic dust.[15]

The probe's ALADDIN instrument (ALDN-S and ALDN-E) measured the variation in dust density[16] while its Gamma-Ray Burst Polarimeter (GAP) measured the polarization of gamma-ray bursts during its six-month cruise.[17]

IKAROS was to be followed by a 40 by 40 metres (130 ft × 130 ft) sail, the Jupiter Trojan Asteroid Explorer, which was intended to journey to Jupiter and the Trojan asteroids, with a proposed goal of returning an asteroid sample to Earth in the 2050s.[18][19][20][21] The Jupiter Trojan Asteroid Explorer was a finalist for Japan's Institute of Space and Astronautical Science (ISAS)' 2nd Large Mission Class. The winning mission was LiteBIRD.

Design

[edit]
IKAROS sail schematic diagram:
  1. (blue square on a line) Tip mass 0.5 kg (1.1 lb), 1 of 4.
  2. (orange rectangle) Liquid crystal device, 1 of 80.
  3. (blue square) Membrane 7.5 μm (0.00030 in) thick, 20 metres (66 ft) on the diagonal.
  4. (black rectangle) Solar cells 25 μm (0.00098 in) thick.
  5. (yellow and blue lines) Tethers.
  6. (blue disc) Main body.
  7. (yellow dots) Instruments.
IKAROS spaceprobe in flight (artist's depiction)

The square sail, deployed via a spinning motion using 0.5-kilogram (1.1 lb) tip masses (key item 1 in figure at right), is 20 m (66 ft) on the diagonal and is made of a 7.5-micrometre (0.00030 in) thick sheet of polyimide (key item 3 in figure at right). The polyimide sheet had a mass of about 10 grams per square metre (0.033 oz/sq ft), resulting in a total sail mass of 2 kilograms (4.4 lb), excluding tip masses, attached panels and tethers. A thin-film solar array is embedded in the sail (key item 4 in figure at right). PowerFilm, Inc. provided the thin-film solar array.[22] Eighty blocks of LCD panels are embedded in the sail,[23] whose reflectance can be adjusted for attitude control (key item 2 in figure at right). The sail also contains eight dust counters on the opposite face as part of the science payload.[24][25]

Mission progress

[edit]

IKAROS was successfully launched together with Akatsuki (the Venus Climate Orbiter) aboard an H-IIA rocket from the Tanegashima Space Center on 21 May 2010.[citation needed]

IKAROS spun at 20–25 revolutions per minute and finished unfurling its sail on 10 June 2010.[26][27][28] The craft contains two tiny ejectable cameras, DCAM1 and DCAM2. DCAM2 was used to photograph the sail after deployment on 14 July 2010.[29]

Acceleration and attitude control (orientation) were successfully tested during the remaining six-month voyage to Venus. On 9 July 2010, JAXA confirmed that IKAROS was being accelerated by its solar sail,[30] and on 23 July announced successful attitude control. Over a 23-hour period of time, the solar angle of the sail was changed by a half a degree, not by using thrusters, but by dynamically controlling the reflectivity of the 80 liquid crystal panels at the outer edge of the sail so that the sunlight pressure would produce torque.[31] IKAROS continues to spin at approximately 2 rpm, requiring the LCD panels to be cycled at that rate for attitude control.[citation needed]

According to JAXA, IKAROS finished all planned experiments in Dec 2010, but the mission continued beyond that date "in order to enhance the skill of controlling solar sail".[32] On 30 November 2012, JAXA announced that IKAROS had been recognized by Guinness World Records as the world's first solar sail spacecraft between planets, and that its two separated cameras, DCAM1 and DCAM2, had been recognized as the smallest size of a spacecraft flying between planets.[33][34] As of 2012, the IKAROS continued to spin, but its attitude control had degraded. This resulted in unexpected sail motions and as a result, downlink through the medium-gain antenna was only intermittently available. The project team was dissolved on 28 March 2013, although a trial receipt of data was planned for a later date.[citation needed]

The project was reactivated on 20 June 2013 in the expectation that the satellite would wake up from a hibernation state as more power from the solar panels became available. The team was able to receive telemetry from the IKAROS between 20 June and 12 September 2013, after which contact was again lost. The loss of contact was around the predicted time of the spacecraft again entering a low-power hibernation mode as power from the solar panels decreased. Available communication time through the Usuda Deep Space Center antenna was limited, so data was gathered only intermittently to estimate the speed, trajectory and rotation of the satellite.[35][36] As of August 2013, acceleration from the IKAROS sail had changed the craft's speed by approximately 400 metres per second (890 mph) in total.[37]

Transmissions were again received on 22 May 2014, the spacecraft flying at a distance of about 230 million kilometers from the Earth. By May 2014, IKAROS was on a ten-month orbit around the Sun, spending seven months of each orbit in hibernation mode due to insufficient power.[38] By 23 April 2015, the spacecraft woke up from hibernation mode for the 4th time and was flying at a distance of about 120 million kilometers from the Earth.[39] On 21 May 2015, JAXA could not receive a signal from IKAROS and concluded that the spacecraft had shifted to the hibernation mode for the fifth time, as expected. Based on the last data received during May 2015, the position of IKAROS at the time was about 110 million kilometers away from the Earth, and about 130 million kilometers from the Sun.[40]

Scientific results

[edit]

From the gamma-ray polarization data of GAP, Toma et al.[41] put a stricter limit on CPT violation. It is an improvement of eight orders of magnitude over previous limits.[42][43]

JAXA scientists stated on 9 July 2010 that the measured thrust force by the solar radiation pressure on IKAROS' 196 m2 sail is 1.12 millinewtons.[44]

See also

[edit]

Notes

[edit]
  1. ^ Mori et al. (2009)
  2. ^ "Small Solar Power Sail Demonstrator "IKAROS"". JAXA. Archived from the original on 30 October 2013. Retrieved 1 October 2010.
  3. ^ a b Stephen Clark (20 May 2010). "H-2A Launch Report – Mission Status Center". Spaceflight Now. Retrieved 21 May 2010.
  4. ^ Samantha Harvey (20 May 2010). "Solar System Exploration: Missions: By Target: Venus: Future: Akatsuki". NASA. Archived from the original on 10 April 2010. Retrieved 21 May 2010.
  5. ^ "IKAROS". Institute of Space and Astronautical Science. Retrieved 30 November 2022.
  6. ^ "IKAROS: Solar Power Sail Demonstrator". ISAS. JAXA. Retrieved 24 May 2015.
  7. ^ "IKAROS enters hibernation mode for 5th time". Small Solar Power Sail Demonstrator "IKAROS" Topics. JAXA. Retrieved 2 March 2019.
  8. ^ "Launch Day of the H-IIA Launch Vehicle No. 17(H-IIA F17)". JAXA. 3 March 2010. Archived from the original on 26 April 2014. Retrieved 5 November 2021.
  9. ^ https://web-japan.org/kidsweb/hitech/icarus/index.html [bare URL]
  10. ^ "今日の IKAROS(12/10) – Daily Report – Dec 10, 2010". IKAROS Blog (in Japanese). JAXA. 10 December 2010. Retrieved 22 January 2011.
  11. ^ "2010年の締めくくり(12/26) – Daily Report – Dec 26, 2010". IKAROS Blog (in Japanese). JAXA. 26 December 2010. Retrieved 22 January 2011.
  12. ^ 宇宙帆船イカロス、お疲れさま…実験終え「人工惑星」に (in Japanese). Asahi Shimbun. 10 December 2010. Retrieved 22 January 2011.[dead link‍]
  13. ^ Mori, Osamu (26 January 2011). "小型ソーラー電力セイル実証機（IKAROS）の定常運用終了報告" (PDF) (in Japanese). JAXA. Retrieved 2 February 2011.
  14. ^ Siddiqi, Asif A. (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF). The NASA history series (second ed.). Washington, DC: NASA History Program Office. p. 2. ISBN 9781626830424. LCCN 2017059404. SP2018-4041.
  15. ^ "小型ソーラー電力セイル実証機「IKAROS（イカロス）」のガンマ線バーストの観測成功について" (in Japanese). JAXA. 14 July 2010. Retrieved 15 July 2010.
  16. ^ Yano, H.; et al. "COSMIC DUST DETECTION BY THE IKAROS-ARRAYED LARGE-AREA DUST DETECTORS IN INTERPLANETARY SPACE (ALADDIN) FROM THE EARTH TO VENUS" (PDF). 42nd Lunar and Planetary Science Conference (2011). Retrieved 14 February 2011.
  17. ^ Yonetoku, D.; et al. (26 October 2010). "Gamma-Ray Burst Polarimeter – GAP – aboard the Small Solar Power Sail Demonstrator IKAROS". Publications of the Astronomical Society of Japan. 63 (3): 625–638. arXiv:1010.5305. Bibcode:2011PASJ...63..625Y. doi:10.1093/pasj/63.3.625.
  18. ^ "IKAROS Project". JAXA. 2008. Archived from the original on 22 September 2008. Retrieved 12 July 2010. The second mission will take place in the late 2010s. It will involve a medium-sized solar power sail with a diameter of 50 metres (160 ft), and will have integrated ion-propulsion engines. The destinations of the spacecraft will be Jupiter and the Trojan asteroids.
  19. ^ SCIENCE AND EXPLORATION IN THE SOLAR POWER SAIL OKEANOS MISSION TO A JUPITER TROJAN ASTEROID. (PDF). T. Okada, T. Iwata, J. Matsumoto, T. Chujo, Y. Kebukawa, J. Aoki, Y. Kawai, S. Yokota, Y. Saito, K. Terada, M. Toyoda, M. Ito, H. Yabuta, H. Yurimoto, C. Okamoto, S. Matsuura, K. Tsumura, D. Yonetoku, T. Mihara, A. Matsuoka, R. Nomura, H. Yano, T. Hirai, R. Nakamura, S. Ulamec, R. Jaumann, J.-P. Bibring, N. Grand, C. Szopa, E. Palomba, J. Helbert, A. Herique, M. Grott, H. U. Auster, G. Klingelhoefer, T. Saiki, H. Kato, O. Mori, J. Kawaguchi. 49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083).
  20. ^ Jeremy Hsu (21 July 2010). "Japan's Solar Sail Is the Toast of Space Science". space.com. Retrieved 8 December 2016.
  21. ^ Shusuke Murai (21 July 2016). "JAXA reveals asteroid probe solar panel". The Japan Times Online. The Japan Times. Retrieved 8 December 2016.
  22. ^ Claire M. Umali (4 May 2010). "Japan tests power of solar sails in deep space". EcoSeed. Archived from the original on 2 December 2010. Retrieved 25 January 2011.
  23. ^ "Small Solar Power Sail Demonstrator 'IKAROS': Successful Attitude Control by Liquid Crystal Device". Japan Aerospace Exploration Agency (JAXA). 23 July 2010.
  24. ^ "Small Solar Power Sail Demonstrator". JAXA. 11 March 2010. Archived from the original on 30 October 2013. Retrieved 7 May 2010.
  25. ^ "IKAROS Project". JAXA. 2008. Archived from the original on 22 September 2008. Retrieved 30 March 2010.
  26. ^ Edwards, Lin (11 June 2010). "IKAROS unfurls first ever solar sail in space". PhysOrg. Retrieved 11 June 2010.
  27. ^ Staff writers (11 June 2010). "Japanese Spacecraft Deploys Solar Sail". Space.com. Retrieved 11 June 2010.
  28. ^ Amos, Jonathan (11 June 2010). "Japan unfurls Ikaros solar sail in space". BBC News. Retrieved 25 January 2011.
  29. ^ Staff writers (16 June 2010). "Mini-camera pictures Japan's Ikaros solar sail". BBC News. Retrieved 17 June 2010.
  30. ^ "About the confirmation of photon acceleration of "IKAROS" the small solar-sail demonstrating craft". JAXA website press release (Press release) (in Japanese). Japan Aerospace Exploration Agency. 9 July 2010. Retrieved 25 January 2011. Graph suggests approx 1.1mN force
  31. ^ "Small Solar Power Sail Demonstrator 'IKAROS'Successful Attitude Control by Liquid Crystal Device" (Press release). Japan Aerospace Exploration Agency (JAXA). 23 July 2010. Retrieved 25 January 2011.
  32. ^ "Solar Power Sail Demonstrator "IKAROS"". Japan Aerospace Exploration Agency (JAXA). Archived from the original on 22 September 2008. Retrieved 30 December 2012.
  33. ^ "IKAROS world record certified!". Japan Aerospace Exploration Agency (JAXA). 30 November 2012. Archived from the original on 30 October 2013. Retrieved 30 December 2012.
  34. ^ "JAXA's solar spacecraft gets Guinness World Records entry". The Asahi Shimbun. 30 December 2012. Archived from the original on 13 February 2013. Retrieved 30 December 2012.
  35. ^ "今日の IKAROS(2013/06/20) – Daily Report – June 20, 2013" (in Japanese). Japan Aerospace Exploration Agency (JAXA). 20 June 2013. Retrieved 8 June 2014.
  36. ^ "今日の IKAROS(12/7) – Daily Report – Dec 7, 2013" (in Japanese). Japan Aerospace Exploration Agency (JAXA). 20 June 2013. Retrieved 8 June 2014.
  37. ^ "今日の IKAROS(8/29) – Daily Report – Aug 29, 2013" (in Japanese). Japan Aerospace Exploration Agency (JAXA). 29 August 2013. Retrieved 8 June 2014.
  38. ^ "IKAROS：3回目の冬眠モード明けについて" (in Japanese). Japan Aerospace Exploration Agency (JAXA). 26 May 2014. Retrieved 8 June 2014.
  39. ^ "IKAROS wakes up from hibernation mode for the 4th time". JAXA. 30 April 2015. Retrieved 24 May 2015.
  40. ^ "IKAROS enters hibernation mode for 5th time". JAXA. 29 May 2015.
  41. ^ Kenji Toma; et al. (December 2012). "Strict Limit on CPT Violation from Polarization of γ-Ray Bursts". Physical Review Letters. 109 (24): 241104. arXiv:1208.5288. Bibcode:2012PhRvL.109x1104T. doi:10.1103/PhysRevLett.109.241104. PMID 23368301. S2CID 42198517.
  42. ^ Michael Schirber (2012). "Synopsis: Distant Bursts Show no Signs of Predicted Light Rotation". Physical Review Letters. 109 (24): 241104. arXiv:1208.5288. Bibcode:2012PhRvL.109x1104T. doi:10.1103/PhysRevLett.109.241104. PMID 23368301. S2CID 42198517.
  43. ^ "Strict Limit on CPT Violation from Gamma-Ray Bursts". Kavli Institute for the Physics and Mathematics of the Universe. 7 December 2012. Archived from the original on 23 March 2013. Retrieved 16 December 2012.
  44. ^ "IKAROS – All News Channel". JAXA. 9 July 2010. Archived from the original on 19 August 2010. Retrieved 24 May 2015.

References

[edit]
[edit]
Wikimedia Commons has media related to IKAROS.
Retrieved from "https://wiki.riteme.site/w/index.php?title=IKAROS&oldid=1262364466"