Hitomi (spacecraft)

Hitomi

300px Artist depiction of Hitomi
Names	ASTRO-H New X-ray Telescope
Mission type	X-ray astronomy
Operator	JAXA
COSPAR ID	2016-012A
SATCAT №	41337
Mission duration	Planned: 3 years Final: 39 days
Spacecraft properties
Launch mass	2,700 kg (6,000 lb)
Dimensions	Length: 14 m (46 ft)
Power	3,500 watts
Start of mission
Launch date	17 February 2016, 08:45 (2016-02-17UTC08:45) UTC
Rocket	H-IIA 202, No. 30
Launch site	Tanegashima Space Center, Japan
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Semi-major axis	6,948.6 km (4,317.7 mi)
Eccentricity	0.0015
Perigee	559.85 km (347.87 mi)
Apogee	581.10 km (361.08 mi)
Inclination	31.01°
Period	96 min
RAAN	67.28°
Argument of perigee	291.82°
Mean anomaly	68.07°
Mean motion	14.99 rev/day
Epoch	27 March 2016, 17:27:54 UTC
Instruments SXS Soft X-ray Spectrometer HXI Hard X-ray Imager SXI Soft X-ray Imager SGD Soft Gamma-ray Detector

Hitomi, also known as ASTRO-H and New X-ray Telescope (NeXT), was an X-ray astronomy satellite commissioned by the Japan Aerospace Exploration Agency (JAXA) for studying extremely energetic processes in the Universe. The space observatory was designed to extend the research conducted by the Advanced Satellite for Cosmology and Astrophysics (ASCA) by investigating the hard X-ray band above 10 keV. The satellite was originally called New X-ray Telescope; at the time of launch it was called ASTRO-H. After it was placed in orbit and its solar panels deployed, it was renamed Hitomi. The new name refers to the pupil of an eye, and to a legend of a painting of four dragons, two of which were given eyes and flew into the sky, and two that were left eyeless and stayed as motionless art. The spacecraft was launched on 17 February 2016 and contact was lost on 26 March 2016 due to multiple incidents with the attitude control system leading to an uncontrolled spin rate and breakup of structurally weak elements.

Objectives

Hitomi's objectives were to explore the large-scale structure and evolution of the universe, as well as the distribution of dark matter within galaxy clusters and how the galaxy clusters evolve over time; how matter behaves in strong gravitational fields (such as matter inspiraling into black holes), to explore the physical conditions in regions where cosmic rays are accelerated, as well as observing supernovae. In order to achieve this, it was designed to be capable of:

1. Imaging and spectroscopic measurements with a hard X-ray telescope;
2. Spectroscopic observations with an extremely high energy resolution using the micro-calorimeter;
3. Sensitive wideband observations over the energy range 0.3-600 keV.

It was the sixth of a series of JAXA X-ray satellites, which started in 1979, and it was designed to observe sources that are an order of magnitude fainter than its predecessor, Suzaku. Its planned mission length was three years. At the time of launch, two other large X-ray satellites were carrying out observations in orbit: the Chandra X-ray Observatory and XMM-Newton, both of which were launched in 1999.

Instruments

The probe carried four instruments and six detectors to observe photons with energies ranging from soft X-rays to gamma rays, with a high energy resolution. Hitomi was built by an international collaboration led by JAXA with over 70 contributing institutions in Japan, the US, Canada, and Europe, and over 160 scientists. With a mass of 2.7 tonnes (2,700 kg), At launch, Hitomi was the heaviest Japanese X-ray mission. The satellite is about 14 m (46 ft) in length.

Two soft X-ray telescopes (SXT-S, SXT-I), with focal lengths of 5.6 m (18 ft), focus light onto a soft X-ray Spectrometer (SXS), provided by NASA, with an energy range of 0.4-12 keV for high-resolution X-ray spectroscopy, and a soft X-ray imager (SXI), with an energy range of 0.3-12 keV.

Two hard X-ray telescopes (HXT), with a focus length of 12 m (39 ft), focus light onto two hard X-ray imagers (HXI), with energy range 5-80 keV, which are mounted on a plate placed at the end of the 6 m (20 ft) extendable optical bench (EOB) that is deployed once the satellite is in orbit. The Canadian Space Agency (CSA) provided the Canadian ASTRO-H Metrology System (CAMS), which is a laser alignment system that will be used to measure the distortions in the extendible optical bench.

Two soft Gamma-ray detectors (SGD), each containing three units, were mounted on two sides of the satellite, using non-focusing detectors to observe soft gamma-ray emission with energies from 60 to 600 KeV.

The Netherlands Institute for Space Research (SRON) in collaboration with the University of Geneva provided the filter-wheel and calibration source for the spectrometer.

Launch

The launch of the satellite was planned for 2013 as of 2008, later revised to 2015 as of 2013. As of early February 2016, it was planned for 12 February, but was delayed due to poor weather forecasts.

Hitomi launched on 17 February 2016 at 08:45 UTC into a low Earth orbit of approximately 575 km (357 mi). The circular orbit had a period of around 96 minutes, and an inclination of 31 degrees. It was launched from the Tanegashima Space Center on board an H-IIA rocket. 14 minutes after launch, the satellite separated from the rocket. The solar arrays later deployed according to plan, and it began its on-orbit checkout.

Loss of communication

On 27 March 2016, JAXA reported that communication with Hitomi had "failed from the start of its operation" on 26 March at 07:40 UTC. On the same day, the U.S. Joint Space Operations Center (JSpOC) announced on Twitter that it had observed a breakup of the satellite into 5 pieces at 08:20 UTC on 26 March 2016, and its orbit also suddenly changed on the same day. Later analysis by the JSpOC found that the fragmentation likely took place around 01:42 UTC, but that there was no evidence the spacecraft had been struck by debris. JAXA received two brief signals from Hitomi on 28 March around 00:00 and 02:30 UTC; by 1 April, a total of four communication events had been detected. It was later determined that these communications were actually not from the satellite as they were on the wrong frequency.

JAXA has stated they were working to recover communication and control over the spacecraft, but that "the recovery will require months, not days." Initially suggested possibilities for the communication loss is that a helium gas leak, battery explosion, or stuck-open thruster caused the satellite to start rotating, rather than a catastrophic failure. JAXA announced on 1 April that Hitomi had lost attitude control at around 19:10 UTC on 25 March. After analysing engineering data from just before the communication loss, however, no problems were noted with either the helium tank or batteries.

The same day, JSpOC released orbital data for ten detected pieces of debris, five more than originally reported, including one piece that was large enough to initially be confused with the main body of the spacecraft. Amateur trackers have observed what is believed to be Hitomi tumbling in orbit, with reports of the main spacecraft body (Object A) rotating once every 1.3 or 2.6 seconds, and the next largest piece (Object L) rotating every 10 seconds.

It was determined that multiple incidents with the attitude control system had caused Hitomi to spin out of control and break up into multiple pieces.

JAXA ceased efforts to restore the satellite on 28 April 2016, switching focus to anomaly investigation. JAXA stated that both solar arrays had likely broken from the spacecraft due to rotation.

In a twist of fate, one of the secondary payloads traveling with Hitomi was ChubuSat-3, a microsatellite dedicated to monitoring global warming effects and space debris.

See also

• List of X-ray space telescopes
• X-ray astronomy

External links

• Hitomi website by JAXA
• Hitomi website by JAXA's Institute of Space and Astronautical Science
• Hitomi website by NASA

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