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Astro-E


Visualization of Astro-E

Astro-E was to be the Japan’s fifth X-ray astronomy mission, but was lost during launch on 10 Feb 2000. Astro-E was developed at the Japanese Institute of Space and Astronautical Science (ISAS) in collaboration with the US and Japanese institutions. Astro-E was to carry, among other instruments, a new type of X-ray spectrometer, the X-ray micro-calorimenter, which would have provided an unprecendent energy resolution compared to non-dispersive instruments.

The mission was rebuild as ASTRO-E2, renamed Suzaku, that was successfully launched in 2005 and operated for 10 years.

Mission Characteristics

Lifetime
10 Feb 2000 (launch failure)
Special Features
First X-ray micro-calorimeter in space

Payload

X-ray Telescope (XRT)

Energy Range
0.2–12 keV
Focal Length
4.75 m (XRT-S)
4.5 m (XRT-I)
Angular Resolution
∼2′
Five nested conical thin-foil grazing incidence telescopes, all gold-coated. Four were XRT-I used for the XIS instrument, the fifth XRT-S served the XRS instrument.

X-ray Spectrometer (XRS)

Energy Range
0.3–12 keV
Effective Area
190 cm2 at 1.5 kev
Field of View
2.9′ × 2.9′
Energy Resolution
∼6.5 eV at 6 keV (FWHM)
An X-ray microcalorimeter composite of 32 pixels at the foci of the XRT-S

X-ray Imaging Spectrometer (XIS)

Energy Range
0.2–12 keV
Effective Area
340 cm2 (FI)
390 cm2 (BI)
Field of View
18′ × 18′
Energy Resolution
130 eV at 6 keV
Four 1024×1024 pixel CCD detectors at the foci of one of the XRT-I. Three are front illuminated (FI), one is back illuminated (BI).

Hard X-ray Detector (HXD)

Energy Range
10–600 keV
Effective Area
∼145 cm2 at 15 keV (PIN)
315 cm2 at 100 keV (GSO)
Field of View
34′ × 34′ (< 100 keV)
4.5° × 4.5° (> 100 keV)
Energy Resolution
3 keV (FWHM) 7.6/(EMeV)0.5 % FWHM
GSO crystal scintillator (>30 keV) & silicon PIN diodes (<60 keV)