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The design and flight performance of the PoGOLite Pathfinder balloon-borne hard X-ray polarimeter

Authors :
Chauvin, M.
Florén, H. -G.
Jackson, M.
Kamae, T.
Kawano, T.
Kiss, M.
Kole, M.
Mikhalev, V.
Moretti, E.
Olofsson, G.
Rydström, S.
Takahashi, H.
Lind, J.
Strömberg, J. -E.
Welin, O.
Iyudin, A.
Shifrin, D.
Pearce, M.
Publication Year :
2015

Abstract

In the 50 years since the advent of X-ray astronomy there have been many scientific advances due to the development of new experimental techniques for detecting and characterising X-rays. Observations of X-ray polarisation have, however, not undergone a similar development. This is a shortcoming since a plethora of open questions related to the nature of X-ray sources could be resolved through measurements of the linear polarisation of emitted X-rays. The PoGOLite Pathfinder is a balloon-borne hard X-ray polarimeter operating in the 25 - 240 keV energy band from a stabilised observation platform. Polarisation is determined using coincident energy deposits in a segmented array of plastic scintillators surrounded by a BGO anticoincidence system and a polyethylene neutron shield. The PoGOLite Pathfinder was launched from the SSC Esrange Space Centre in July 2013. A near-circumpolar flight was achieved with a duration of approximately two weeks. The flight performance of the Pathfinder design is discussed for the three Crab observations conducted. The signal-to-background ratio for the observations is shown to be 0.25$\pm$0.03 and the Minimum Detectable Polarisation (99% C.L.) is (28.4$\pm$2.2)%. A strategy for the continuation of the PoGOLite programme is outlined based on experience gained during the 2013 maiden flight.<br />Comment: Accepted for publication in Experimental Astronomy. 26 pages, 20 figures

Details

Database :
arXiv
Publication Type :
Report
Accession number :
edsarx.1508.03345
Document Type :
Working Paper
Full Text :
https://doi.org/10.1007/s10686-015-9474-x