The AMS-02 experiment will be installed on the International Space Station at an altitude of about 400 km in 2010 to measure for three years cosmic rays. The total acceptance including the electromagnetic calorimeter is 0.095 m$^2$sr. This work focuses on the anticoincidence counter system (ACC). The ACC is a single layer composed of 16 interlocking scintillator panels that surround the tracker inside the inner bore of the superconducting magnet. The ACC needs to detect particles that enter or exit the tracker through the sides with an efficiency of better than 99.99 %. This allows to reject particles that have not passed through all the subdetectors and may confuse the charge and momentum measurements which is important for an improvement of the antinuclei-measurements. In 2007/2008 all subdetectors were integrated into the AMS-02 experiment and atmospheric muons were collected. These data were used to determine the ACC detection efficiency.
Deep Dive into The Anticoincidence Counter System of AMS-02.
The AMS-02 experiment will be installed on the International Space Station at an altitude of about 400 km in 2010 to measure for three years cosmic rays. The total acceptance including the electromagnetic calorimeter is 0.095 m$^2$sr. This work focuses on the anticoincidence counter system (ACC). The ACC is a single layer composed of 16 interlocking scintillator panels that surround the tracker inside the inner bore of the superconducting magnet. The ACC needs to detect particles that enter or exit the tracker through the sides with an efficiency of better than 99.99 %. This allows to reject particles that have not passed through all the subdetectors and may confuse the charge and momentum measurements which is important for an improvement of the antinuclei-measurements. In 2007/2008 all subdetectors were integrated into the AMS-02 experiment and atmospheric muons were collected. These data were used to determine the ACC detection efficiency.
arXiv:0906.1068v1 [astro-ph.IM] 5 Jun 2009
PROCEEDINGS OF THE 31st ICRC, Ł ´OD´Z 2009
1
The Anticoincidence Counter System of AMS-02
Ph. von Doetinchem∗, Th. Kirn∗, K. L¨ubelsmeyer∗and St. Schael∗
∗I. Physics Institute B, RWTH Aachen University, Sommerfeldstr. 14, 52074 Aachen, Germany
Abstract. The AMS-02 experiment will be installed
on the International Space Station at an altitude of
about 400 km in 2010 to measure for three years
cosmic rays. The total acceptance including the
electromagnetic calorimeter is 0.095m2sr.
This work focuses on the anticoincidence counter
system (ACC). The ACC is a single layer composed of
16 interlocking scintillator panels that surround the
tracker inside the inner bore of the superconducting
magnet. The ACC needs to detect particles that
enter or exit the tracker through the sides with
an efficiency of better than 99.99 %. This allows
to reject particles that have not passed through all
the subdetectors and may confuse the charge and
momentum measurements which is important for an
improvement of the antinuclei-measurements.
In 2007/2008 all subdetectors were integrated into
the AMS-02 experiment and atmospheric muons
were collected. These data were used to determine
the ACC detection efficiency.
Keywords: AMS-02, Veto, Inefficiency
I. THE AMS-02 DETECTOR
The AMS-02 experiment will be installed on the In-
ternational Space Station at an altitude of about 400 km
in 2010 for about three years to measure cosmic rays
without the influence of the Earth’s atmosphere [1].
The detector consists of several subdetectors for the
determination of the particle properties, namely a tran-
sition radiation detector (TRD), a time of flight system
(TOF), a cylindrical silicon microstrip tracker with eight
layers surrounded by an anticoincidence counter system
(ACC) in a superconducting magnet with a field of 0.8 T
strength, a ring image ˇCerenkov detector (RICH) and an
electromagnetic calorimeter (ECAL) (fig. 1).
II. THE ANTICOINCIDENCE COUNTER
The AMS-02 anticoincidence counter [2], [3] sur-
rounds the silicon tracker and can be used as a veto for
the trigger decision made by the TOF (fig. 2, upper).
This is important for rejecting events with particles
entering the detector from the side or with particles from
secondary interactions inside the detector which could
distort the charge measurement. To improve existing
upper limits on antihelium an inefficiency of the ACC
smaller than 10−4 is needed according to MC simula-
tions. The inefficiency is the ratio of missed to the total
number of particle tracks crossing the ACC.
Another important task of the ACC is to reduce the
trigger rate during periods of very large flux, e.g. in the
Fig. 1.
The AMS-02 detector.
South Atlantic Anomaly. For that purpose, it is important
to use a detector with a fast response.
The ACC cylinder has a diameter of 1.1 m and a
height of 0.83 m and is made out of 16 scintillation
panels (Bicron BC-414) with a thickness of 8 mm. The
ultraviolet scintillation light through ionization losses
of charged particles is absorbed by wavelength shifting
fibers (WLS, Kuraray Y-11(200)M) which are embedded
into the panels. The WLS fibers are coupled to clear
fiber cables (Toray PJU-FB1000) for the final light
transport to photomultiplier tubes (Hamamatsu R5946).
A set of two panels is read out by the same two
photomultipliers, one on top and one on the bottom, via
clear fiber cables (Y-shape) in order to have redundancy
and to save weight (fig. 2, lower). The slot between
two panels is realized with tongue and groove and is
crucial for the determination of the inefficiency because
of less scintillator material and a smaller active (WLS) to
passive (scintillator) material ratio. The qualification of
the individual components is discussed in references [2],
[3].
III. ACC INEFFICIENCY DETERMINATION WITH
ATMOSPHERIC MUONS
AMS-02 was pre-integrated with all subsystems but
the magnet in 2007 and 2008 at CERN, Geneva. The
data used here are taken after this installation.
2
PH. VON DOETINCHEM et al. THE ACC OF AMS-02
Fig. 2.
Upper) The anticoincidence counter system after integration (left) and the principle of component arrangement (right). Lower) ACC
working principle.
In most runs a trigger is given by any two out of
the four TOF planes. The trigger condition for events
used in this analysis used tracks with hits in both upper
TOF layers. TRD and tracker tracks are extrapolated to
the ACC in order to find the intersection on the ACC
cylinder and to determine the ACC detection efficiency.
A. Event Reconstruction
Fig. 3 shows a typical event used in the following
analysis. In addition, the AMS-02 coordinate system is
shown. The origin is located at the center of the tracker.
The axis of symmetry of the ACC cylinder is the same
as the z axis of the AMS-02 coordinate system.
A track fit was developed to find tracks which point
to the ACC. The requirement of a reasonable agreement
between TRD and tracker track acts as an effective
momentum filter such that onl
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