Vibration isolation system for cryocoolers on the XRISM
We discuss the design and performance of the vibration isolation system (VIS) used for the Resolve microcalorimeter on the X-Ray Imaging and Spectroscopy Mission (XRISM) spacecraft. Resolve makes high spectral resolution observations of celestial X-rays. XRISM was conceived as a recovery mission following the short-lived Hitomi mission. As such, the design of Resolve is similar to that of the soft X-ray spectrometer (SXS). A VIS was initially developed for the Hitomi SXS after discovering that vibrations from the cryocooler degraded the sensor’s performance. However, the VIS for Resolve was completely redesigned to include a hold-and-release mechanism to avoid damage to the compressor during launch or ground-based sine-vibe tests. The XRISM spacecraft was successfully launched in September 2023, confirming the functionality of the VIS while in orbit.
Authors
- Yoh Takei (ORCID: https://orcid.org/0000-0003-2517-3904)
- Susumu Yasuda (ORCID: https://orcid.org/0009-0001-2905-3291)
- Keiichi Yanagase (ORCID: https://orcid.org/0000-0002-6138-9246)
- Seiji Yoshida (ORCID: https://orcid.org/0000-0001-8311-6612)
- Kazuki Watanabe
- Atsushi Okamoto (ORCID: https://orcid.org/0000-0003-2725-9189)
Institutions
- Sumitomo Heavy Industries (Japan) (JP)
- Japan Aerospace Exploration Agency (JP)
Publication Details
- Journal
- Journal of Astronomical Telescopes Instruments and Systems
- Published
- 2025-03-12
- DOI
- https://doi.org/10.1117/1.jatis.11.4.042004
- Citations
- 1
- Primary Topic
- Advanced Thermodynamic Systems and Engines
- Type
- article
- Field-Weighted Citation Impact
- 0.71