The design and performance of the XL-Calibur anticoincidence shieldVisa övriga samt affilieringar
Antal upphovsmän: 342023 (Engelska)Ingår i: Nuclear Instruments and Methods in Physics Research Section A: Accelerators, Spectrometers, Detectors and Associated Equipment, ISSN 0168-9002, E-ISSN 1872-9576, Vol. 1048, artikel-id 167975Artikel i tidskrift (Refereegranskat) Published
Abstract [en]
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.
Ort, förlag, år, upplaga, sidor
2023. Vol. 1048, artikel-id 167975
Nyckelord [en]
Anticoincidence, BGO scintillator, Photomultiplier tube, X-ray polarimetry, Scientific ballooning, Monte Carlo, Qualification testing
Nationell ämneskategori
Annan teknik Maskinteknik Astronomi, astrofysik och kosmologi
Identifikatorer
URN: urn:nbn:se:su:diva-218370DOI: 10.1016/j.nima.2022.167975ISI: 000995686300001Scopus ID: 2-s2.0-85146099547OAI: oai:DiVA.org:su-218370DiVA, id: diva2:1776761
2023-06-282023-06-282023-10-20Bibliografiskt granskad