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The design and performance of the XL-Calibur anticoincidence shield

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arxiv 2212.04139 v1 pith:E6SLTAIU submitted 2022-12-08 astro-ph.IM physics.ins-det

The design and performance of the XL-Calibur anticoincidence shield

classification astro-ph.IM physics.ins-det
keywords shieldanticoincidencedesignperformancebackgroundmeasuredmissionpolarimeter
verification ladder T0 review T1 audit T2 compute T3 formal T4 reserved
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The XL-Calibur balloon-borne hard X-ray polarimetry mission comprises a Compton-scattering polarimeter placed at the focal point of an X-ray mirror. The polarimeter is housed within a BGO anticoincidence shield, which is needed to mitigate the considerable background radiation present at the observation altitude of ~40 km. This paper details the design, construction and testing of the anticoincidence shield, as well as the performance measured during the week-long maiden flight from Esrange Space Centre to the Canadian Northwest Territories in July 2022. The in-flight performance of the shield followed design expectations, with a veto threshold <100 keV and a measured background rate of ~0.5 Hz (20-40 keV). This is compatible with the scientific goals of the mission, where %-level minimum detectable polarisation is sought for a Hz-level source rate.

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