Performance verification of the Suzaku X-ray Spectrometer in the flight configuration

Details Performance verification of the Suzaku X-ray Spectrometer in the flight configuration Performance verification of the Suzaku X-ray Spectrometer in the flight configuration

Apr 2006

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006nimpa.559..614o&link_type=abstract

Nuclear Instruments and Methods in Physics Research Section A, Volume 559, Issue 2, p. 614-616.

Physics

1

Scientific paper

The X-ray Spectrometer (XRS) is a high resolution, non-dispersive cryogenic detector on board the X-ray satellite, Suzaku (Astro-E2), which was successfully launched on July 10, 2005. The XRS achieves an energy resolution of 6 eV at 6 keV (FWHM) and covers a broad energy range of ˜0.07 10 keV. The XRS will enable powerful plasma diagnostics of a variety of astrophysical objects such as the dynamics of gas in clusters of galaxies. The XRS was integrated to the spacecraft in September 2004, and underwent a series of spacecraft tests until April 2005. We describe results of the XRS performance verification in the spacecraft configuration. First, the noise level was extremely low on the spacecraft, and most of the pixels achieved an energy resolution of 5 6 eV at 5.9 keV. Microphonic noise from the mechanical cooler was one of the concerns, but this was not a problem, when the dewar was integrated to the spacecraft and filled with solid neon. To attain the best energy resolution, however, correction of gain drift is mandatory. The XRS has a dedicated calibration pixel for that purpose, and drift correction using the calibration pixel is very effective when the gain variation is due to changes in the ˜60mK heat sink temperature. On the other hand, the calibration pixel and the other pixels do not respond in the same way to variations of the helium and neon bath temperatures, and this effect requires further study.

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