Akatsuki (あかつき, 暁, "Dawn"), also known as the Venus Climate Orbiter (VCO) and Planet-C, is a Japanese (JAXA) space probe tasked to study the atmosphere of Venus. It was launched aboard an H-IIA 202 rocket on 20 May 2010, and failed to enter orbit around Venus on 6 December 2010. After the craft orbited the Sun for five years, engineers placed it into an alternative elliptical Venusian orbit on 7 December 2015 by firing its attitude control thrusters for 20 minutes.
Artist's concept of the Akatsuki spacecraft in orbit around Venus
|Mission type||Venus orbiter|
JAXA Special Site
~2 years (science phase)|
elapsed: 8 years, 4 months and 4 days
|Manufacturer||NEC Space Technologies|
|Launch mass||517.6 kg (1,141 lb)|
|Dry mass||320 kg (710 lb)|
|Dimensions||1.04 m × 1.45 m × 1.44 m (3.4 ft × 4.8 ft × 4.7 ft)|
|Power||>700 watts at 0.7 AU|
|Start of mission|
|Launch date||20 May 2010, 21:58:22UTC|
|Launch site||Tanegashima YLP-1|
|Pericytherion||1,000 kilometers (620 mi)|
|Apocytherion||330,000 kilometers (210,000 mi)|
|Flyby of Venus (failed insertion)|
|Closest approach||6 December 2010, 23:49:00 UTC|
|Distance||550 kilometers (340 mi)|
|Orbital insertion||7 December 2015|
By using five different cameras working at several wavelengths, Akatsuki is studying the stratification of the atmosphere, atmospheric dynamics, and cloud physics. Astronomers working on the mission reported detecting a possible gravity wave that occurred on Venus in December 2015.
Akatsuki is a Japanese space mission to the planet Venus. Planned observations include cloud and surface imaging from an orbit around the planet with cameras operating in the infrared, visible and UV wavelengths to investigate the complex Venusian meteorology. Other experiments are designed to confirm the presence of lightning and to determine whether volcanism occurs currently on Venus. In most planets, the atmosphere circulates much slower than the rotation speed of the planet. However, on Venus, while the planet rotates at 6 km/h at the equator, the atmosphere spins around the planet at 300 km/h.
Akatsuki is Japan's first planetary exploration mission since the failed Mars orbiter Nozomi probe which was launched in 1998. Akatsuki was originally intended to conduct scientific research for two or more years from an elliptical orbit around Venus ranging from 300 to 80,000 km (190 to 49,710 mi) in altitude, but its alternate orbit had to be highly elliptical ranging between 1,000 km and 10,000 km at its nearest point and about 360,000 km at its farthest. This larger orbit takes 10 days to complete instead of the originally planned 30 hours. The budget for this mission is ¥14.6 billion (US$174 million) for the satellite and ¥9.8 billion (US$116 million) for the launch.
The main bus is a 1.45 × 1.04 × 1.44 m (4.8 × 3.4 × 4.7 ft) box with two solar arrays, each with an area of about 1.4 m2 (15 sq ft). The solar arrays provide over 700 W of power in Venus orbit. The total mass of the spacecraft at launch was 517.6 kg (1,141 lb). The mass of the science payload is 34 kg (75 lb).
Propulsion is provided by a 500-newton (110 lbf) bi-propellant, hydrazine-dinitrogen tetroxide orbital maneuvering engine and twelve mono-propellant hydrazine reaction control thrusters, eight with 23 N (5.2 lbf) of thrust and four with 3 N (0.67 lbf). It is the first spacecraft to use a ceramic (silicon nitride) retrofire thruster. The total propellant mass at launch was 196.3 kg (433 lb).
Communication is via an 8 GHz, 20-watt X-band transponder using the 1.6 m (5 ft 3 in) high-gain antenna. The high-gain antenna is flat to prevent heat from building up in it. Akatsuki also has a pair of medium-gain horn antennas mounted on turntables and two low-gain antennas for command uplink. The medium-gain horn antennas are used for housekeeping data downlink when the high-gain antenna is not facing Earth.
- the Lightning and Airglow Camera (LAC) is looking for lightning in the visible spectrum (552-777 nm)
- the ultraviolet imager (UVI) is studying the distribution of specific atmospheric gases such as sulfur dioxide in ultraviolet wavelengths (293–365 nm)
- the longwave infrared camera (LIR) is studying the structure of high-altitude clouds at a wavelength where they emit heat (10 μm)
- the infrared 1 μm camera (IR1) is imaging heat radiation emitted from Venus's surface rocks (0.90–1.01 μm) and help researchers to spot active volcanoes, if they exist. Status: active.
- the infrared 2 μm camera (IR2) studied heat radiation emitted from the middle to lower atmosphere (1.65–2.32 μm) (Unavailable for observation after December 2016 due to an electronic failure.)
- the Ultra-Stable Oscillator (USO) for high precision measurement of distance and communication
A public relations campaign was held between October 2009 and January 2010 by the Planetary Society and JAXA, to allow individuals to send their name and a message aboard Akatsuki. Names and messages were printed in fine letters on an aluminium plate and placed aboard Akatsuki. 260,214 people submitted names and messages for the mission. Around 90 aluminium plates were created for the spacecraft, including three aluminium plates in which the images of the Vocaloid Hatsune Miku and her super deformed figure Hachune Miku were printed.
Akatsuki left the Sagamihara Campus on 17 March 2010, and arrived at the Tanegashima Space Center's Spacecraft Test and Assembly Building 2 on 19 March. On 4 May, Akatsuki was encapsulated inside the large payload fairing of the H-IIA rocket that launched the spacecraft, along with the IKAROS solar sail, on a 6-month journey to Venus. On 9 May, the payload fairing was transported to the Tanegashima Space Center's Vehicle Assembly Building, where the fairing was mated to the H-IIA launch vehicle itself.
Orbit insertion failureEdit
Akatsuki was planned to initiate orbit insertion operations by igniting the orbital maneuvering engine at 23:49:00 on 6 December 2010 UTC. The burn was supposed to continue for twelve minutes, to an initial Venus orbit with an apoapsis of 180,000 to 200,000 km (110,000 to 120,000 mi), a periapsis of 550 km (340 mi), and a four-day orbital period.
The orbit insertion maneuver was confirmed to have started on time, but after the expected blackout due to occultation by Venus, the communication with the probe did not recover as planned. The probe was found to be in safe-hold mode, spin-stabilized state with ten minutes per rotation. Due to the low communication speed through the low-gain antenna, it took a while to determine the state of the probe. JAXA stated on 8 December that the probe's orbital insertion maneuver had failed. At a press conference on 10 December, officials reported that Akatsuki's engines fired for less than three minutes, far less than what was required to enter into Venus orbit. Further research found that the likely reason for the engine malfunction was salt deposits jamming the valve between the helium pressurization tank and the fuel tank. As a result, engine combustion became oxidizer-rich, with resulting high combustion temperatures damaging the combustion chamber throat and nozzle. A similar vapor leakage problem destroyed the NASA Mars Observer probe in 1993.
As a result, the probe was in a heliocentric orbit, rather than Venus orbit. Since the resulting orbit had an orbital period of 203 days, shorter than Venus' orbital period of 225 days, the probe drifted around the Sun compared to Venus.
JAXA developed plans to attempt another orbital insertion burn when the probe returned to Venus in December 2015. This required placing the probe into "hibernation" or safe mode to prolong its life beyond the original 4.5-year design. JAXA expressed some confidence in keeping the probe operational, pointing to reduced battery wear, since the probe was then orbiting the Sun instead of its intended Venusian orbit.
Telemetry data from the original failure suggested that the throat of its main engine, the orbit maneuver engine (OME) was still largely intact, and trial jet thrusts of the probe's onboard OME were performed twice, on 7 and 14 September 2011. However, the thrust was only about 40 newtons (9.0 lbf), which was 10% of expectations. Following these tests, it was determined that insufficient specific impulse would be available for orbital maneuvering by the OME. It was concluded that the remaining combustion chamber throat was completely destroyed by transient ignition of the engine. As a result, the selected strategy was to use four hydrazine attitude control thrusters, also called reaction control system (RCS), to drive the probe into orbit around Venus. Because the RCS thrusters do not need oxidiser, the remaining 65 kg of oxidiser (MON) was vented overboard in October 2011 to reduce the mass of the spacecraft.
Three peri-Venus orbital maneuvers were executed on 1 November, 10 and 21 November 2011 using the RCS thrusters. A total delta-v of 243.8 m/s was imparted to the spacecraft. Because the RCS thrusters' specific impulse is low compared to the specific impulse of the OME, the previously planned insertion into low Venusian orbit became impossible. Instead, the new plan was to place the probe in a highly elliptical orbit with an apoapsis of a hundred thousand kilometers and a periapsis of a few thousand kilometers from Venus. Engineers planned for the alternate orbit to be prograde (in the direction of the atmospheric super-rotation) and lie in the orbital plane of Venus. The method and orbit were announced by JAXA in February 2015, with an orbit insertion date of 7 December 2015. The probe reached its most distant point from Venus on 3 October 2013 and had been approaching the planet since then.
After performing the last of a series of four trajectory correction maneuvers between 17 July and 11 September 2015, the probe was established on a trajectory to fly past Venus on 7 December 2015, when Akatsuki would make a maneuver to enter Venus orbit after a 20-minute burn with four thrusters that were not rated for such a hefty propulsive maneuver. Instead of taking about 30 hours to complete an orbit around Venus—as was originally planned—the new orbit targeted would place Akatsuki in a nine-day orbit after an adjustment in March 2016.
After JAXA engineers measured and calculated its orbit following the December 7 orbital insertion, JAXA announced on December 9 that Akatsuki had successfully entered the intended elliptical orbit, as far as 440,000 km (270,000 mi) from Venus, and as close as 400 km (250 mi) from Venus's surface with an orbital period of 13 days and 14 hours.
A follow-up thruster burn on 26 March 2016 lowered Akatsuki's apoapsis to about 330,000 km (210,000 mi) and shortened its orbital period from 13 to 9 days.
The orbiter started its two-year period of "regular" science operations in mid-May 2016. Since 9 December 2016, the near-infrared 2-μm camera has been unavailable for observations due to an electronic failure. Its 1-μm camera, long-wave infrared camera, ultraviolet imager, and lightning and airglow camera continue normal operation.
By April 2018, Akatsuki finished its regular observation phase, and entered an extended operation phase.
Soon after insertion in December 2015 and in "a few glimmers in April and May" 2016 the craft's instruments recorded a "bow-shape feature in the atmosphere stretching 6,000 miles, almost pole to pole — a sideways smile". Scientists on the project termed the feature a "gravity wave" in the planet's winds above Aphrodite Terra, "a highland region about the size of Africa that rises up to three miles from the surface". The mission has collected data in all relevant spectral bands from far-ultraviolet (FUV) to microwave wavelengths.
Images from the Akatsuki orbiter revealed something similar to jet stream winds in the low and middle cloud region, which extends from 45 to 60 kilometers in altitude. The wind speed maximized near the equator. In September 2017 JAXA scientists named this phenomenon 'Venusian equatorial jet'. They also published results on equatorial winds at cloud-top level by tracking clouds on the UV spectrum.
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- "Japanese probe fires thrusters in second bid to enter Venus orbit". The Japan Times. 7 December 2015. Retrieved 7 December 2015.
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- Initial products of Akatsuki 1-μm camera Archived 3 June 2018 at the Wayback Machine.. Earth, Planets and Space. 2018, vol. 70, nbr. 6. doi:10.1186/s40623-017-0773-5
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- JAXA's press briefing, 22:00, 7 December 2010 JST
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- "AKATSUKI: Orbit successfully controlled". PLANET-C Team/JAXA. 5 August 2015. Retrieved 10 September 2015.
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- Overview of useful spectral regions for Venus: An update to encourage observations complementary to the Akatsuki mission. Icarus. Volume 288, 15 May 2017, Pages 235–239
- Bouic, Damia (16 January 2018). "A new look at Venus with Akatsuki". The Planetary Society Blog. The Planetary Society. Retrieved 2018-01-28.
- "Venus: Jet-setting atmosphere". Japan Aerospace Exploration Agency (JAXA). 5 September 2017. Retrieved 2017-09-26.
- Mean winds at the cloud top of Venus obtained from two-wavelength UV imaging by Akatsuki. Takeshi Horinouchi, Toru Kouyama, Yeon Joo Lee, Shin-ya Murakami, Kazunori Ogohara, Masahiro Takagi, Takeshi Imamura, Kensuke Nakajima, Javier Peralta, Atsushi Yamazaki, Manabu Yamada and Shigeto Watanabe. Earth, Planets and Space doi:10.1186/s40623-017-0775-3 Published: 15 January 2018.
- Hunt for optical lightning flash in Venus using LAC onboard Akatsuki spacecraft. Takahashi, Yukihiro; Sato, Mitsuteru; Imai, Masataka. 19th EGU General Assembly, EGU2017, proceedings from the conference held 23–28 April 2017 in Vienna, Austria., p.11381.
|Wikimedia Commons has media related to Akatsuki (spacecraft).|
- Venus Climate Orbiter Akatsuki official website
- JAXA Akatsuki Planet-C page
- JAXA Akatsuki Special Site
- Planet-C page (Solar Terrestrial Physics Group)
- Detailed Space Review article about Akatsuki and its recovery
- Venus Climate Orbiter Akatsuki (PDF, 1.72 Mb)
- Akatsuki - List of scientific publications