Suzaku (formerly ASTRO-EII) was an X-ray astronomy satellite developed jointly by the Institute of Space and Aeronautical Science at JAXA and NASA's Goddard Space Flight Center to probe high energy X-ray sources, such as supernova explosions, black holes and galactic clusters. It was launched on 10 July 2005 aboard the M-V launch vehicle on the M-V-6 mission. After its successful launch, the satellite was renamed Suzaku after the mythical Vermilion bird of the South.[4]
![]() A picture of a fully integrated Astro-E2 before vibration tests at ISAS/JAXA. | |
Names | ASTRO-EII |
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Mission type | Astronomy |
Operator | JAXA / NASA |
COSPAR ID | 2005-025A ![]() |
SATCAT no. | 28773 |
Website | www |
Mission duration | 2 years (planned) 10 years 1 month 23 days (achieved) |
Spacecraft properties | |
Spacecraft type | ASTRO |
Bus | ASTRO-E |
Manufacturer | Toshiba[1] |
Launch mass | 1,706 kg (3,761 lb) [2] |
Dimensions | 2 metres x 5 metres |
Power | 500 watts |
Start of mission | |
Launch date | 10 July 2005, 03:30:00 UTC |
Rocket | M-V # 6 |
Launch site | Uchinoura Space Center, Uchinoura, Kagoshima |
End of mission | |
Deactivated | 2 September 2015 |
Decay date | No earlier than 2020 [3] |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Low Earth orbit |
Perigee altitude | 550 km (340 mi) |
Apogee altitude | 550 km (340 mi) |
Inclination | 31° |
Period | 96 minutes |
Instruments | |
X-ray Spectrometer-2 (XRS-2) X-ray Imaging Spectrometer (XIS) Hard X-ray Detector (HXD) | |
![]() The M-V launch vehicle carrying ASTRO-E veering off course after launch on 10 February 2000. | |
Mission type | Astronomy |
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Operator | Institute of Space and Astronautical Science (ISAS) / NASA |
COSPAR ID | 2005-025A ![]() |
SATCAT no. | 28773![]() |
Mission duration | Failed to orbit |
Spacecraft properties | |
Spacecraft type | ASTRO |
Bus | ASTRO-E |
Manufacturer | Toshiba |
Launch mass | 1600 kg |
Dimensions | 2 metres x 5 metres |
Power | 500 watts |
Start of mission | |
Launch date | 10 February 2000, 01:30:00 UTC |
Rocket | M-V # 4 |
Launch site | Kagoshima Space Center |
End of mission | |
Decay date | Failed to orbit |
Orbital parameters | |
Reference system | Geocentric orbit (planned) |
Regime | Low Earth orbit |
Perigee altitude | 550 km (340 mi) |
Apogee altitude | 550 km (340 mi) |
Inclination | 31.0° |
Period | 96.0 minutes |
Instruments | |
X-ray Spectrometer (XRS) X-ray Imaging Spectrometer (XIS) Hard X-ray Detector (HXD) X-ray Telescope (XRT) | |
Just weeks after launch, on 29 July 2005, the first of a series of cooling system malfunctions occurred. These ultimately caused the entire reservoir of liquid helium to boil off into space by 8 August 2005. This effectively shut down the X-ray Spectrometer-2 (XRS-2), which was the spacecraft's primary instrument. The two other instruments, the X-ray Imaging Spectrometer (XIS) and the Hard X-ray Detector (HXD), were unaffected by the malfunction. As a result, another XRS was integrated into the Hitomi X-ray satellite, launched in 2016.
On 26 August 2015, JAXA announced that communications with Suzaku had been intermittent since 1 June 2015, and that the resumption of scientific operations would be difficult to accomplish given the spacecraft's condition.[5] Mission operators decided to complete the mission imminently, as Suzaku had exceeded its design lifespan by eight years at this point. The mission came to an end on 2 September 2015, when JAXA commanded the radio transmitters on Suzaku to switch themselves off.[3][6]
Suzaku carried high spectroscopic resolution, very wide energy band instruments for detecting signals ranging from soft X-rays up to gamma-rays (0.3–600 keV). High resolution spectroscopy and wide-band are essential factors to physically investigate high energy astronomical phenomena, such as black holes and supernova. One such feature, the K-line (x-ray), may be key to more direct imaging of black holes.
Suzaku was a replacement for ASTRO-E, which was lost in a launch failure. The M-V launch vehicle on the M-V-4 mission launched on 10 February 2000 at 01:30:00 UTC but experienced a failure 42 seconds later, failing to achieve orbit and crashing with its payload into the Indian Ocean.[8]
Suzaku discovered "fossil" light from a supernova remnant.[9]
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Astronomical observation |
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Private miniaturized satellites |
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Explorers Program | |||
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List of Explorers Program missions | |||
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Proposals |
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← 2004 · Orbital launches in 2005 · 2006 → | |
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Deep Impact | Kosmos 2414 · Universitetsky-Tatyana | AMC-12 | USA-181 | XTAR-EUR · Maqsat-B2 (Sloshsat-FLEVO) | Himawari 6 | Progress M-52 (TNS-0) | XM-3 | Inmarsat-4 F1 | Ekspress AM-2 | USA-165 | Apstar 6 | Soyuz TMA-6 | DART | Spaceway 1 | USA-182 | Cartosat-1 · HAMSAT | NOAA-18 | DirecTV-8 | Foton-M No.2 | Progress M-53 | Molniya-3K No.12 | Cosmos 1 | Intelsat Americas 8 | Ekspress AM-3 | Shijian 7 | Suzaku | STS-114 (Raffaello MPLM) | FSW-21 | Thaicom 4 | MRO | Kirari · Reimei | Monitor-E | FSW-22 | Kosmos 2415 | Progress M-54 (RadioSkaf) | Anik F1R | USA-183 | Soyuz TMA-7 | CryoSat | Shenzhou 6 | Syracuse 3A · Galaxy 15 | USA-186 | Beijing-1 · TopSat · Sina-1 · SSETI Express (CubeSat Xi-V · UWE-1 · nCUBE-2) · Mozhaets-5 · Rubin-5 | Inmarsat-4 F2 | Venus Express | Spaceway-2 · Telkom-2 | Gonets-M No.1 · Kosmos 2416 | Meteosat 9 · INSAT-4A | Kosmos 2417 · Kosmos 2418 · Kosmos 2419 | GIOVE-A | AMC-23 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in parentheses. |