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The Time of Flight System of the AMS-02 Space Experiment

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arxiv hep-ex/0111096 v1 pith:ZDQJXRY5 submitted 2001-11-30 hep-ex

The Time of Flight System of the AMS-02 Space Experiment

classification hep-ex
keywords fieldams-02willchargedetectorelectronicsinstalledspace
verification ladder T0 review T1 audit T2 compute T3 formal T4 reserved
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The Time-of-Flight (TOF) system of the AMS detector gives the fast trigger to the read out electronics and measures velocity, direction and charge of the crossing particles. The new version of the detector (called AMS-02) will be installed on the International Space Station on March 2004. The fringing field of the AMS-02 superconducting magnet is $1.0\div2.5$ kG where the photomultiplers (PM) are installed. In order to be able to operate with this residual field, a new type of PM was chosen and the mechanical design was constrained by requiring to minimize the angle between the magnetic field vector and the PM axis. Due to strong field and to the curved light guides, the time resolution will be $150\div180$ ps, while the new electronics will allow for a better charge measurement.

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