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Nuclear Instruments and Methods in Physics Research A 522 (2004) 360370
Manufacturing the Schmidt corrector lens for the
Pierre Auger Observatory
M.A.L. de Oliveira*, V. de Souza, H.C. Reis, R. Sato
Departamento de Raios C!osmicos e Cronologia (DRCC), Instituto de F!sica Gleb Wataghin (IFGW), Universidade Estadual de
Campinas (UNICAMP), Observat !orio Pierre Auger, Cx.P. 6165, CEP 13084-971, Campinas-SP, Brazil
Received 14 August 2003; received in revised form 24 November 2003; accepted 26 November 2003
Abstract
The Pierre Auger Observatory is designed to provide measurements of Extensive Air Showers initiated in the upper
atmosphere by cosmic rays with energies greater than 1018 eV: One of the employed techniques is air fluorescencedetectors with UV filters and a corrector lens. We describe in this article the production process of the corrector lens in
Brazil, starting from the design of the machines up to the final tests in the prototype telescope. We have used diamond
grinding tools to shape a ring of corrector lens with inner radius of 85 cm and outer radius of 110 cm ; divided in 24segments and with aspherical shape. After the production of a first complete set of segments, we measured a segment
shape scanning with a laser. The lens was then installed at the telescope and we measured its overall influence on the
spot size, taking pictures of the Vega star.
r 2003 Elsevier B.V. All rights reserved.
PACS: 96.40.z; 96.40.Pq
Keywords: Cosmic rays showers; Fluorescence detectors; Corrector lenses
1. Introduction
The Pierre Auger Observatory [1] is a large
international effort to try to solve one of the most
puzzling mysteries of nature that has appeared inthe last times: the Ultra High Energy Cosmic Rays
(UHECRs). These cosmic rays are subatomic
particles going through the universe and reaching
Earth with macroscopic energy B1020 eVB16 J:How can these particles gain such tremendous
energy? This is one of the questions that the Pierre
Auger Observatory is aiming to answer. Cosmic
rays with energies above 5 1019 eV were first
observed in 1962 by Linsley [2] in the Volcano
Ranch array. Since then, several events withenergy above 1020 eV have been observed [35].
However, the present arrays, with collecting area
o100 km2; do not provide enough statistics, dueto the extremely low flux (1 event century1km2)
in this energy region [6,7]. The explanation of these
events face theoretical difficulties, since it is
believed to exist a cutoff in the spectra of cosmic
rays around 5 1019 eV due to the interac-
tion with 2:7 K primordial photons, the GZKcutoff [8,9].
ARTICLE IN PRESS
*Corresponding author. Tel.: +55-1937885276; fax: +55-
1937885512.
E-mail address: [email protected] (M.A.L. de Oliveira).
0168-9002/$- see front matterr 2003 Elsevier B.V. All rights reserved.doi:10.1016/j.nima.2003.11.409
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The observatory is a hybrid giant detector using
two different techniques: water Cherenkov tanks
and fluorescence telescopes. The first technique
consists of an array of 1600 tanks separated by1:5 km spread over an area of 3000 km2: TheUHECRs are so rare that even with such a large
area, extrapolating the AGASA spectrum [10]
below 1020 eV; we will have approximately 103events/year. Some advantages of the Cherenkov
tanks are their low cost and the fact that this kind
of detector can operate continuously with any kind
of weather. The ground array samples the lateral
distribution of the shower generated by the
primary UHECRs. The second technique consists
of 24 telescopes overseeing the array of tanks.
These telescopes observe the fluorescence light
emitted by the air nitrogen molecules when they
are excited by the particles of an Extensive Air
Showers (EAS). They operate with clean weather
in moonless nights. This condition corresponds to
only 10% of the available time, but this disadvan-
tage is compensated by the crucial information
that the fluorescence detector gives to us: the
longitudinal distribution profile of the EAS. This
information is used in order to determine the
energy, the arrival direction and to estimate
the composition of the UHECR that originatedthe showers. Each one of the 24 telescopes is
composed by a spherical mirror with 30 30
field of view reflecting the fluorescence light on an
array of 440 photomultiplier tubes (PMTs). The
system adopts Schmidt optics in order to reduce
coma aberration. The basic setup was thought to
have an aperture box consisting of a 85 cm
diaphragm radius to exclude distant off-axis
rays and a band pass filter passing the
300 nmolo410 nm band, which contains the
main emission peaks of the nitrogen fluorescence.However, it was proposed that the inclusion of a
corrector ring in the outer radius part of the
diaphragm would increase the collection area of
the telescopes, increasing the signal to noise ratio
without significant loss in resolution. The logic for
such a design is spelled out in the next section.
Simulations have shown [11] that the use of a
corrector ring would increase the collection area
significantly, still keeping the aberration within the
specified value of 0:5 (which is one-third of the
PMT aperture for the Auger fluorescence tele-
scope). Indeed, it was possible to determine the
most suitable shape of the corrector ring lenses, as
discussed in Ref. [11]. Here, we start from theresults described in this paper and explain the steps
given for the construction of the first prototype
ring, from the machine conception to the final tests
of the sample lenses.
2. Lens construction
The Fluorescence Detector telescopes uses
Schmidt optics following the proposal in [12] and
are sets of spherical mirrors of 340 cm of curvature
radius with a diaphragm limiting the coma
aberration. Due to the telescope geometry, the
spots at the focal surface have spherical aberra-
tions. Their intensity is proportional to the
effective collecting area A and the noise is
proportional to the square root of this quantity,
in such a way that the signal to noise ratio S=N isgiven by
S
Np
ffiffiffiffiA
O
r1
where O is the solid angle covered by a PMT pixel.The diaphragm is introduced to cut rays far
away from the optical axis, avoiding the coma
aberration [13] and allowing a wider field of view
in comparison with a normal telescope.
As the S=N ratio can change with both mirrorand PMTs diameter, one can increase the mirror
diameter or decrease the PMTs pixel diameter to
increase the S=N ratio, but anyone of suchsolutions would raise too much the costs. Thus,
for the designed mirror values (340 cm of curva-
ture radius and 30
30
of aperture) the spotsachieve the required resolution (0:5 diameter inthe focal surface) for a 85 cm diaphragm radius.
The idea of a corrector lens appeared as a way
to increase the telescope area, increasing the spot
luminosity, without increasing the spot size in
excess. The shape of a ring has been chosen instead
of a filled lens to reduce the final cost and because
the simulations showed that it was needed to
correct only the rays beyond 85 cm from the main
optical axis. It has been decided to increase the
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diaphragm radius in 25 cm: Taking into accountthe glass transmittance and losses through the
segment borders, we calculated an overall light loss
of about 20% within the corrector ring. Then,including the shadow of the PMT camera, the
effective collection is 86% larger for an incident
beam parallel to the telescope optical axis 0 and
63% larger for an incident beam inclined of 20
with respect to the telescope optical axis. For
further details, see the reference [11].
In Fig. 1 is shown the geometry of one segment
of the corrector ring, the studied unit vector
normal to the curved surface ~nn and its projec-tions along cylindrical symmetry axes. The graph
in Fig. 2 shows the limits within which the radial
component of the normal vector ~nnr should lie[12], taking into account the chromatic aberra-
tions, which is discussed in the Appendix A.
Some profiles were suggested by the collabora-
tion [14,15] in an attempt to simplify the produc-
tion (see Fig. 3). The comparison of these profiles
with the previous studied limits is also given in Fig.
2. For the circular approximation, case A, the lens
surface is a toroid which goes through itself, in this
plot is a straight line passing through the point
0:8 m; 0: We can see that the lens profile cannot
be approximated by a spherical surface in thewhole segment extension. However, in the case B,
a part of the profile is out of the allowed region,
then the spot size that the telescope will produce
using this type of lens is larger than the required
0:5 0:5 as is written in Ref. [15]. In the case A,it seems to be good enough though a small part of
the profile is out of the allowed region: this
happens because we considered the spot size as
the circle that contains 100% of the light [11],
while in the Ref. [14] it was taken for 90% of thelight. However, our calculation (using 100% of the
light) is more restrictive.
One way to produce lenses for the Schmidt
telescopes is by a vacuum method [16] in which
one deforms a parallel plate and grinds a spherical
surface while the glass is bent. However, we could
not use this method because the deformation
would break the plate that we were using, made
of optical glass. Other difficulty in manufacturing
the lens is its size (220 cm in external diameter).
ARTICLE IN PRESS
Fig. 1. Illustration of the lens surface normal and its
projections.
Fig. 2. Radial projection of the normal unitary vector, nr; tothe curved surface as a function of the distance, r; to the
telescope axis. We compare the limits to maintain the spotresolution with the two proposed profiles (as discussed in
Fig. 3) and the curve produced by our machine.
Fig. 3. Proposed lens profiles for the corrector ring: case A by
Palatka [14] and case B by Cordero [15].
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The problem is not only the machine to produce
this huge lens but also to obtain the appropriate
material and transportation to the site. To solve
these problems the lens was divided in 24 segments
(following the suggestion by Paul Sommers). Fig. 4
shows the layout of each segment. A problem that
appeared with segmentation was the fact that the
center of symmetry is far away from each piece
that could make its production more difficult.One way to solve these problems was suggested
by the enterprise Schwantz Ltd1 that proposed a
machine with a circular base to hold all the 24
segments. The circular base rotates around its
central axis and a circular tool (a disk with small
abrasive diamond cylinders) grinds the material.
Only one edge of this disk is in contact with the
glass. Considering that the position of the tool,
the material and the base are rigidly positioned,
the profile that such machine can produce is shown
in Fig. 2 (see Appendix B). The machine profiledepends on the position, orientation and the
diameter of the tool. The diameter of the tool
was chosen to be 35 cm for two reasons: Schwantz
has technical problems to produce larger tools and
it is impossible to produce the desired surface
profile with a smaller tool (see Fig. 15b and
Ref. [11]).
The process starts with rectangular 296
307 12 mm3 BK7 glass plates from Schott2.
First, one surface is ground and polished to
become as plane as possible using a planning
machine. The planning machine is constituted by a
needle that controls the position and orientation of
a grinding disk with about 20 cm in diameter and
the glass plate rotates around its center. With the
friction between glass plate and grinding disk, thisdisk rotates and grinds the plate almost homo-
geneously. This process does not produce a really
plane surface but it is good enough for our
purposes: deviation of the normal is around
2 mrad:Then the glass is cut to the shape (see Fig. 4) and
is put on the machine to make the profile. The
machine (as illustrated in Fig. 5) was constructed
at Schwantz considering the described ideas. The
base disk can be controlled to spin with a period in
the range of 340 min: The grinding disk isconnected directly to its motor axis and the motorto a base which allows to control the orientation
and the position of the disk by screws. The
frequency of the grinding disk is of about
700 rpm: The produced profile was controlledduring grinding process measuring the curvature
of the surface with a spherometer.
ARTICLE IN PRESS
Fig. 4. The project of the corrector ring segments.
1Schwantz Ferramentas Diamantadas e Com!ercio !Optico
Ltda, Indaiatuba, Brazil. 2Schott Glaswerke, Mainz, Germany.
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However, a problem appeared using this system
(probably because the system is not rigid): the
produced surface had small furrows (see Fig. 6).
Then, another tool was introduced to correct these
defects. It is composed of an iron plate which has
approximately the shape of one lens segment with
grinding pastilles of aluminum oxide. It accom-
modates under the plate and makes pseudo-random movements on the glass while the base
makes a revolution in about 10 min: Before usingthis tool, the produced surface of the lens is copied
putting a sandpaper on the corrector ring surface
while the tool performs the pseudo-random move-
ments on the sandpaper (see Fig. 6).
After all these steps the segments need to be
polished, what is done by both correction tools,
but replacing the diamond cylinders by felts. The
whole process takes about 180 man-hours for the
production of an entire corrector ring, with seven
manual interventions between each step. Although
approximately 75% of this time is consumed by
the grinding machine which is autonomous.
3. Lenses tests
After the completion of the lenses production,
we have performed tests to measure their surfaces
profiles. These tests were done with a laser
scanning method and with a CCD image of a
star, as we will describe below.
3.1. Laser method
When a beam of light impinges on a surface
separating two media with different refraction
indices, it splits in two beams: the reflected and the
refracted. Therefore, impinging a beam on the lens
segment we can see three beams: two going
backward and one going forward, relatively to
the incident beam. This happens because the beam
that goes in the lens can undergo multiple
reflections before getting out the lens. Measuring
the direction of the incident and of the outgoingbeams we can obtain the normal of the lens
surfaces and the lens profile.
In Fig. 7, we have a layout of the system that
was used to study the lens profile. A diode laser
was used as the light source, S; whose wavelengthis between 635 and 670 nm: On the screen, A1; wemeasured the positions, R1 and R2; with amillimeter paper. The scan method consists in
varying the impinging position, L1; on the firstsurface, S1; and reading the arriving points, R1
ARTICLE IN PRESS
Fig. 5. Design of the constructed machine to produce the
curved profile of the lens.
Fig. 6. Left: illustrates the furrows that appeared in the lens
using only the griding disk; Right: shows the system used to
copy the lens profile to the pseudo-random movement tool.
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and R2; on the screen. To make easier themeasurements of the positions L1; we put a paperwith holes of 1 mm of diameter along the lens
x-axis.
Unfortunately, the source has an undesirable
angular divergence (of about 0:5 cm after apropagation of 400 cm). This gives an additional
uncertainty in the measured positions R1 and R2
and consequently in the lens profile. The way wehave treated these uncertainties is described below.
We aligned the system, making the beam to turn
back on itself, restricting the incident light to
propagate on the plane x z: A reference point onscreen A1 was adopted averaging two adjacent
reflections to the laser shadow. With the positions
S; L1 and R1 we can obtain the direction of theincident ~ii S~LL1 and of the reflected ~rr1 L1~RR1 beams. The direction of the normal to thesurface S1 is
~nn1p~rr1
jj~rr1 jj ~ii
jj~iijj: 2
Measuring the normal in some points of the
surface S1 we can obtain its profile. Almost
the same approach can be used to get the profile
of the plane surface, S2; with S; L1 and R2; nowconsidering the direction of the incident and
reflected light inside the lens using the direction
~nn1 ; obtained in the previous step. We adopted arefraction index of 1.514 for the BK7 glass2 to
reconstruct the data, which is the value for the
center of the laser wavelengths band. The main
uncertainties of the laser method come from the
angular divergence of the source. This was treatedby a Monte Carlo method in the following way: we
took randomly distributed points within the spots,
according to a Gaussian distribution with mean
equal to the center of gravity of the spot and
standard deviation given by the spot divergence,
i.e., the points were sorted within S7DS;L17DL1; R17DR1 and R27DR2 and we calcu-lated the normal unit vectors of each surface, n1and n2: We repeated this process several times andwe got a distribution of n1 and n2 for a given
measured datum. The results for n1 and n2 and the
statistical uncertainties are presented in Fig. 8. The
graph of Fig. 8 is a plot in a general reference
system defined by the laboratory walls. We can see
that the component in y-axis of both surfaces
almost vanishes along all segment. It means that
the produced profile is almost symmetric, as
desirable. The other component (x) seems to
follow a straight line. So, as x projection is
changing, we can say that these surfaces have
approximately circular profile, similar to what was
proposed by Palatka (see Fig. 3) where the
curvature radius can be obtained as C dnr=dr
1: As the alignment of lens segment hasbeen done with the reflected light going back to the
source, the plane surface S2 does not coincide with
the plane x y: Consequently, we cannot comparedirectly these results with Fig. 2. But, we must
rotate the results to the frame in which the average
normal of the surface S2 is pointing in the
direction of z- and x-axis is pointing along the
radial direction of lens segment. The new plane
x y of this frame should be very near the plane in
which the segment was holding on the machineduring the production process.
Fig. 9 shows the results for the curved surface of
four segments. The full lines show the limits, given
by the simulation, within which the data must be
and the dotted line is the profile that the machine
should produce if everything (disk tool, base and
glass) were rigid and assuming the following
parameters: R 97:5 cm; rc 17:5 cm; yr 1:10 and yf 1:07
(see Appendix B, Fig. 14,
for their definitions). We can see that the data fit
ARTICLE IN PRESS
Fig. 7. Scanning the surfaces S1 and S2 of the lens with a laser
at the light source S: The reflections R1 and R2 on the screenA1; as well as L1 and S; are used in the ray-tracing
reconstruction.
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very well in the region from 87.5105 cm: Wethink that the disagreement near the edges of the
lens (or outside the region described above) is
mainly due to the introduction of the second
header (random movement header). But, as we will
see further in the next test, this problem does not
poses us serious difficulties. The curvature radiusof the lens can be calculated as the inverse of the
inclination of the line which best describe the data:
C1 dnr=dr: Fitting the available data of Fig. 9in the range 90 cmoro103 cm; we can calculateC 64075 cm:
3.2. Star picture at the Auger telescope
This test was done using the Auger Fluorescence
Telescope in Malarg .ue, Argentina. The data was
ARTICLE IN PRESS
Fig. 9. Data: resulting profiles of four samples shifted by about
90o within the ring (the segments are numbered from 1 to 24 for
the full ring); full curves: the allowed limits given by the
simulation and; dashed line: the best fit for the machine curve.
The errors are smaller than 0.44 in the same ordinate scale.
Fig. 8. Normal unit vectors components as a function of the distance to the diaphragm center for a sample segment. On the left side is
given the projections ofn1 (normal to the curved surface) and on the right side the projections of n2 (normal to the plane surface). In
each sub-figure the projections are designated in the upper left box.
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taken during four nights of March 2002. During
this period the Vega star was in the field of view of
the telescope. Vega (Alpha Lyrae) is a star of
spectral class A0V, with zero magnitude and arelatively flat electromagnetic spectrum within the
wavelengths 350850 nm: The test consisted ontaking pictures with a CCD camera of the star
image formed at the focal surface. The light of the
star enters the system through the aperture
window and is reflected by the mirror into the
camera surface. The camera is covered with a white
UV reflecting screen. The CCD camera is placed in
front of the mirrors aimed at the screen so that we
can get the image of the star (see Fig. 10).
Our intention was to take several pictures of the
star and to determine the spot size of its image in
the camera surface. This measurement was crucial
to quantify the quality of the whole telescope setup
by establishing the total influence of the corrector
ring on the spot size.
In order to increase the S=N ratio avoiding themotion of the star in the camera field of view, we
took 32 pictures of the star in 8 s exposure time
each in two telescopes configurations: without
corrector ring (85 cm of aperture diaphragm
radius) and corrector ring only. For the latter
setup, we masked the inner 85 cm of the aperturein order to get only light that passed through the
lenses. Fig. 11 shows the superposition of the 32
pictures of Vega in both cases.
The analysis procedure consisted in measuring
the light integral as a function of the distance from
the star center. This can be seen in Fig. 12 where it
is possible to notice the effect of the corrector ring.
In each case, the light intensity was normalized to
the own total amount. The light that enters the
telescope passing through the lenses is concen-
trated in the center of the spot while the lightcoming from the inner part of the aperture is
spread in a larger area. The full line in the plot
shows the concentration of light for the total
aperture of the telescope (radius of 1:1 m) with thecorrector ring in place. The figure shows the good
corrector ring performance, approximately 95% of
the light through the corrector ring will end within
the 0:75 cm spot radius, which corresponds to thespecified value of 0:5; or one third of the PMTpixel size.
ARTICLE IN PRESS
Fig. 10. Taking pictures of Vega spot image with a CCD
camera.
Fig. 11. Superpositions of Vega pictures without corrector ring
(above) and with corrector ring only (below).
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4. Conclusion
We described in this article the production of
the corrector ring for the aperture system of the
Pierre Auger Fluorescence Detector. Starting from
its conception and supported by a ray tracing
simulation [11], where the limits of the projections
of one lens surface normal over the another were
established, we detailed the proposals and the
implemented process, describing the machine thathas been constructed to produce the ring. After the
production was completed, we tested some sample
segments by direct laser scanning and the whole
ring by star picture. In the first test, we achieved
the lens profile of one surface, as produced by the
machine, while in the last we evaluated the overall
performance of the corrector ring working to-
gether with one telescope at the site. The results
show that the segments were within the specifica-
tions and that it was possible to increase the
collection area of the detector without increasingthe spherical aberrations.
Acknowledgements
We would like to thank Carlos O. Escobar Paul
Sommers, Hans Klages, Rog!erio Marcon, Ant-#onio C. da Costa and Emerson Schwantz for
important contributions on many aspects of this
work. This work was supported by FAPESP and
CNPq (Brazil).
Appendix A. Chromatic aberration
Let nr be the radial component of the normal to
the curved lens surface and suppose that the plane
surface has its normal along the #z-axis, the allowed
values for nrr were studied in Ref. [11]. As the
lens profile, in that work, was calculated with a
specific refraction index, the chromatic aberrations
were not taken into account. However, we know
that there will be a variation in the refraction index
in the allowed UV filter region of wavelengths. In
the case of the used glass (BK7), the refraction
index ranges from 1:550 to 1.528 (from the shortestto the longest wavelengths). Thus, one needs to
calculate the limits for each refraction index value,
as shown in Fig. 13. So, our goal is reached if we
guarantee that the surface profile is in the region
between the continuous upper line and the dashed
lower line. These limits are adopted throughout
this work.
Appendix B. Lens profile produced by a circulartool
The surface defined by the revolution around
the position O of the circumference with radius rc
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Fig. 13. Chromatic aberration: the limits within which the lens
profile should be produced for the correspondings refraction
indices for l 410 nm n1 and l 300 nm n2:
Fig. 12. Light integral of Vega pictures. This plot determines
the spot size of the telescope configuration.
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and which is in the plane that pass through the
point ~RR and the normal ~nn (see Fig. 14) may bedescribed by the height z and distance r from the
position O since the surface has cylindrical
symmetry.
If we had ~nnp#y we would obtain a toroidalsurface described by equation is z2 r R2 r2c ;that is the profile proposed by Palatka et al. [14]
(see Fig. 3A) with rc 838:3 cm and R 79:527 cm:
Indeed, we would like to analyze the surfaceproduced when the normal ~nn is almost parallel tothe #z-axis. In order to do this, we calculated the
position of the points of the disk writing the
component z as function ofr to a given ~nn; R and rc:With these points we calculated numerically dz=drand then the radial component of the normal,
using the expression of Ref. [11]
zr z0
Zrr0
nrr0
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 nrr
0
2q dr
0 B:1
In Fig. 15 we have some of these surfaces within
the tolerance limits for the lens profiles. We can see
that the overall surface is moved byWR when we
change R to R WR (Fig. 15a), while decreasing
(increase) rc the profile becomes more curved
(straight) in the graphic nrr (Fig. 15b). The others
two graphics show how the direction ~nn changes theprofile.
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Fig. 14. System to produce lens profile using a disk with
radius rc:
0.85 0.9 0.95 1 1.05 1.1
-50
-40
-30
-20
-10
0 std
R+
R-
Limits
1000Xn
r
r(m)(a)
1000Xn
r
r(m)
(b)
0.85 0.9 0.95 1 1.05 1.1
-50
-40
-30
-20
-10
0 std
-n
+n
Limits
1000Xn
r
r(m)(c)
1000X
nr
r(m)
(d) 0.85 0.9 0.95 1 1.05 1.1-50
-40
-30
-20
-10
0
0.85 0.9 0.95 1 1.05 1.1-50
-40
-30
-20
-10
0 std
r+
r-
Limits
std
-n
+n
Limits
Fig. 15. Surface profiles produced by the system of Fig. 14
with different parameters. All the graphics show the two
limits of the lens profiles and std the surface produced with
parameters R 0:975 m; rc 0:175 m and normal compo-nents of plane of disk nr 0:021 and ny 0:015: Otherprofiles are identified as x7 means that the parameter x was
changed x-x7Wx; where WR 0:025 m; Wr 0:025 m;Wnr 0:005 and Wny 0:005:
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ARTICLE IN PRESS
M.A.L. de Oliveira et al. / Nuclear Instruments and Methods in Physics Research A 522 (2004) 360370370
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