Vibration isolation system for cryocoolers of soft x-ray spectrometer on-board ASTRO-H (Hitomi)

Abstract. The soft x-ray spectrometer (SXS) onboard ASTRO-H (named Hitomi after launch) is a microcalorimeter-type spectrometer, installed in a dewar to be cooled at 50 mK. The energy resolution of the SXS engineering model suffered from microvibration from cryocoolers mounted on the dewar. This is mitigated for the flight model (FM) by introducing vibration isolation systems between the cryocoolers and the dewar. The detector performance of the FM was verified before launch of the spacecraft in both ambient condition and thermal-vacuum condition, showing no detectable degradation in energy resolution. The in-orbit detector spectral performance and cryocooler cooling performance were also consistent with that on ground, indicating that the cryocoolers were not damaged by launch environment. The design and performance of the vibration isolation system along with the mechanism of how the microvibration could degrade the cryogenic detector is shown. Lessons learned from the development to mitigate unexpected issues are also described.

[1]  David A. Naylor,et al.  Safari: instrument design of the far-infrared imaging spectrometer for spica , 2017, International Conference on Space Optics.

[2]  S. Oguri,et al.  Mission Design of LiteBIRD , 2013, 1311.2847.

[3]  Ryuichi Fujimoto,et al.  Performance of the helium dewar and cryocoolers of ASTRO-H SXS , 2016, Astronomical Telescopes + Instrumentation.

[4]  Jelle de Plaa,et al.  The X-ray Integral Field Unit (X-IFU) for Athena , 2013, Astronomical Telescopes and Instrumentation.

[5]  Ryuichi Fujimoto,et al.  Development status of the mechanical cryocoolers for the Soft X-ray Spectrometer on board Astro-H , 2014 .

[6]  Ryuichi Fujimoto,et al.  Vibration isolation system for cryocoolers of Soft X-ray Spectrometer (SXS) onboard ASTRO-H (Hitomi) , 2016, Astronomical Telescopes + Instrumentation.

[7]  Naoko Iwata,et al.  Thermal Control System of X-ray Astronomy Satellite ASTRO-H: Current Development Status and Prospects , 2014 .

[8]  Ryuichi Fujimoto,et al.  The Astro-H high resolution soft x-ray spectrometer , 2016, Astronomical Telescopes + Instrumentation.

[9]  Hideyuki Mori,et al.  ASTRO-H Soft X-ray Telescope (SXT) , 2011, Astronomical Telescopes and Instrumentation.

[10]  Yoshiharu Namba,et al.  The ASTRO-H (Hitomi) x-ray astronomy satellite , 2016, Astronomical Telescopes + Instrumentation.

[11]  Regis P. Brekosky,et al.  The design, implementation, and performance of the Atro-H SXS calorimeter array and anti-coincidence detector , 2016, Astronomical Telescopes + Instrumentation.

[12]  Kosei Ishimura,et al.  Ground based test verification of a nonlinear vibration isolation system for cryocoolers of the Soft X-ray Spectrometer (SXS) onboard ASTRO-H (Hitomi) , 2017, 2017 IEEE Aerospace Conference.

[13]  Ryuichi Fujimoto,et al.  In-flight performance of the Soft X-ray Spectrometer detector system on Astro-H , 2016, Astronomical Telescopes + Instrumentation.

[14]  F. S. Porter,et al.  System design and implementation of the detector assembly for the Astro-H soft x-ray spectrometer , 2016, Astronomical Telescopes + Instrumentation.

[15]  Kosei Ishimura,et al.  DUAL STAGE ISOLATION – A PASSIVE BI-LINEAR APPLICATION FOR LAUNCH LOAD ATTENUATION AND ON-ORBIT JITTER MITIGATION , 2017 .

[16]  Ryuichi Fujimoto,et al.  The Suzaku High Resolution X-Ray Spectrometer , 2007 .

[17]  Ryuichi Fujimoto,et al.  In-orbit operation of the ASTRO-H SXS , 2016, Astronomical Telescopes + Instrumentation.

[18]  Ryuichi Fujimoto,et al.  Flight model performance test results of a helium dewar for the soft X-ray spectrometer onboard ASTRO-H , 2016 .

[19]  Yoh Takei,et al.  Evaluation of In-Orbit Thermal Performance of X-Ray Astronomy Satellite "Hitomi" , 2017 .