In-flight performance of the XRISM/Resolve detector system
The Resolve instrument was launched on-board the XRISM observatory in early September 2023. The Resolve spectrometer is based on a high-sensitivity X-ray calorimeter detector system that has been successfully deployed in many ground and sub-orbital spectrometers. However, the Resolve instrument will be the first long-term implementation in space. The instrument will provide essential diagnostics for nearly every class of X-ray emitting objects, from the atmosphere of Jupiter to the outskirts of galaxy clusters, without degradation for spatially extended objects. The Resolve detector system consists of a 36-pixel microcalorimeter array operated at a heat-sink temperature of 50mK. In pre-flight testing, the detector system demonstrated a resolving power of better than 1300 at 6 keV with a simultaneous bandpass from below 0.3 keV to above 12 keV and a timing precision better than 100 μs. An anti-coincidence detector placed directly behind the microcalorimeter array effectively suppresses background. The detector energy-resolution budget included terms for interference from the Resolve cooling system and the spacecraft. Additional terms for energy-scale stability, on-orbit effects, and use of mid-grade events were also included, predicting an end-of-life, on-orbit performance for high and mid-grade events that meets the requirement of 7 eV FWHM at 6 keV. Here we discuss the actual on-orbit performance of the Resolve detector system and compare this to performance in pre-flight testing, on-orbit predictions, and the almost identical Hitomi/SXS instrument. We will also discuss the on-orbit gain stability, any additional on-orbit interference, and measurements of the on-orbit background.
Authors
- Yoshiaki Kanemaru (ORCID: https://orcid.org/0000-0002-4541-1044)
- Ryuichi Fujimoto (ORCID: https://orcid.org/0000-0002-2374-7073)
- Gary A. Sneiderman
- Megan E. Eckart (ORCID: https://orcid.org/0000-0003-3894-5889)
- Renata Cumbee (ORCID: https://orcid.org/0000-0001-9894-295X)
- Masahiro Tsujimoto (ORCID: https://orcid.org/0000-0002-9184-5556)
- Yoshitomo Maeda (ORCID: https://orcid.org/0000-0002-9099-5755)
- Kosuke Sato (ORCID: https://orcid.org/0000-0001-8754-5975)
- Maurice A. Leutenegger (ORCID: https://orcid.org/0000-0002-3331-7595)
- F. S. Porter (ORCID: https://orcid.org/0000-0002-6374-1119)
- Misaki Mizumoto (ORCID: https://orcid.org/0000-0003-2161-0361)
- Yoshitaka Ishisaki (ORCID: https://orcid.org/0000-0003-0163-7217)
- S. Yamada (ORCID: https://orcid.org/0000-0003-4808-893X)
- Yuusuke Uchida (ORCID: https://orcid.org/0000-0002-7962-4136)
- Caroline A. Kilbourne (ORCID: https://orcid.org/0000-0001-9464-4103)
- Richard L. Kelley (ORCID: https://orcid.org/0009-0007-2283-3336)
- Meng P. Chiao
- Tomomi Watanabe
- Makoto Sawada
- Yoh Takei
Institutions
- Lawrence Livermore National Laboratory (US)
- Goddard Space Flight Center (US)
- Rikkyo University (JP)
- Tokyo University of Science (JP)
- University of Teacher Education Fukuoka (JP)
- Japan Aerospace Exploration Agency (JP)
- Tokyo Metropolitan University (JP)
- Saitama University (JP)
Publication Details
- Published
- 2024-08-21
- DOI
- https://doi.org/10.1117/12.3018882
- Citations
- 17
- Primary Topic
- Superconducting and THz Device Technology
- Type
- article
- Field-Weighted Citation Impact
- 5.64