Spacecraft n°: |
Japanese satellite n°: 127 |
The satellite has been renamed "Akari" after launch.
Launch data:
| Designation | 28939 / 06005A |
| Launch date | 21 Feb 2006 - 21:28 UT |
| Launch site | Uchinoura |
| Launch vehicle |
M-5 (2) |
| Mission | Government: Scientific Research Astronomy |
| Sun-Synchronous LEO Earth orbit on: |
| Perigee / Apogee | 707 x 716 km |
| Eccentricity | 6.35E-04 |
| Inclination | 98.2° |
| Period | 99.2 min |
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Spacecraft data:
| Prime contractor | Japan Aerospace Exploration Agency (JAXA) |
| Operator | JAXA / ISAS |
| Platform | |
| Mass at launch | 952 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| Equipment | 70 cm IR telescope |
| Design lifetime | 1.5 yrs |
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Decay:
| Out of service: | 31 July 2012 |
| Cause: | |
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The satellite has completed standalone tests and was connected onto the 3rd stage of the M-V-8 rocket. Function tests after the connection was also went successfully.
Description:
ASTRO-F, originally named IRIS (InfraRed Imaging Surveyor), is a 70 cm cooled
telescope. It has a much more powerful capability for survey work than the IRAS, owing to the
advanced technologies now available:
- ASTRO-F covers wide wavelength range from K-band to 200 µm. ASTRO-F will
perform an all-sky survey at wavelengths > 50 µm using high-sensitivity
Ge:Ga detector arrays. In the near- and mid-infrared ranges, large-format
arrays are employed for a deep sky survey in selected sky regions.
- The sensitivity of ASTRO-F is much higher than that of the IRAS. For example,
the ASTRO-F has 50-100 times higher sensitivity at 100 µm and more than 1000
times at mid-infrared wavelengths.
- ASTRO-F has a diffraction-limited angular resolution at wavelengths longer
than 10 µm. The pixel sizes of ASTRO-F are less than 1 arcmin even at 100-200
µm, several times smaller than the beam of the IRAS.
- ASTRO-F has capabilities for low-resolution spectroscopy. In the near- and
mid-infrared ranges, spectroscopy using prisms is available. The
Fourier-transform spectrometer is used for the wavelength range from 50 to 200
µm. This capability is very important for classification of sources detected
in the deep survey, rough determination of the redshift, etc.
Mission details:
- Japan launched the ASTRO-F infrared astronomy satellite at 21:28 UTC on
Feb 21. ASTRO-F separated from the M-V-8 rocket final stage in a 301 x
718 km x 98.2 deg orbit; it will use an onboard propulsion system to
reach its final orbit and then will eject its optics cover.
The satellite has been named "Akari" (light). By Mar 3 it was in a
707 x 716 km x 98.2 deg orbit; this had been adjusted to
695 x 710 km by Mar 16. Because of attitude control problems,
ejection of the optics cover has been delayed until mid-April.
- Akari carries a 0.67m-diameter liquid-helium-cooled infrared telescope
with detectors ranging from the near infrared to 60 and 170 micron
channels in the far IR. It will carry out the first far infrared sky
survey since IRAS in 1983.
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Ref.: #6n, #7(JR562), #14, #226 - update: 15.10.12
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