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Total absorption scintillation spectrometer
Item Type text; Thesis-Reproduction (electronic)
Authors Kielkopf, Edward C., 1933-
Publisher The University of Arizona.
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TOTAL ABSORPTION SCINTILLATION SPECTROMETER
by
Edward C. Kielkopf» Jr.
A Thesis Submitted to the Faculty of the
DEPARTMENT OF NUCLEAR ENGINEERING
In Partial Fulfillment of the Requirements For the Degree of
MASTER OF SCIENCE
In the Graduate College
THE UNIVERSITY OF ARIZONA
1 9 6 7
STATEMENT BY AUTHOR
This thesis has been submitted in partial fulfillment of requirements for an advanced degree at The University of Arizona and is deposited in the University Library to be made available to borrowers under rules of the Library.
Brief quotations from this thesis are allowable without special permission, provided that accurate acknowledgment of source is made. Requests for permission is extended quotation from or reproduction of this manuscript in whole or in part may be granted by the head of the major department or-the Dean of the Graduate College when in his judgment the proposed use of the material is in the interests of scholarship. In all other instances, however, permission must be obtained from the author.
SIGNED
APPROVAL BY THESIS DIRECTOR
This thesis has been approved on the data shown below:
ROY G. POST Professor of Nuclear Engineering
Date
ACKNOWLEDGMENTS
The author wishes to express his appreciation to Dr. Roy G. Post
and Dr. Morton E. Wacks for their guidance and assistance in accomplish
ing this work. The help of Dr. Monte V. Davis and Dr. Robert L. Seale
is gratefully acknowledged.
He would like to thank Mr. Donald M« Fiehl for his. work in pro
ducing the machined components of the system.
A special note of thanks is due the author*s wife and children
for their encouragement and patience while this work was being performed.
Finally, he extends his appreciation to the United States Army
for the opportunity to complete this work.
iii
TABLE OF CONTENTS
Page
LIST OF ILLUSTRATIONS ........................................ . v
ABSTRACT ....... vi
INTRODUCTION ............. 1
THEORY......................... 3
Gamma Radiation...... 3Background Radiation ............ 5Scintillation Spectrometry........ 7
THE TOTAL ABSORPTION PROBLEM ............... 9
Large Crystals .............................. 11Anticoincidence Shielding ................................... 12Sum Coincidence ..... 16
SYSTEM DESIGN AND CONSTRUCTION ................................. 19
OPERATION ....... 30
CONCLUSION ........................ 33
APPENDIX .................................................. 35
LIST OF REFERENCES ........... 41
iv
LIST OF ILLUSTRATIONS
Figure ^age
1 Absorption Cross Sections for Gamma Radiationof Nal (Tl) ........................................ 6
2 Cobalt 60 Spectra Using a 4 3/4 x 5 1/2 inchNal (Tl) Well Crystal . ............................ 10
3 Block Diagram of Anticoincidence ScintillationSpectrometer ....... 13
4 An Anticoincidence Scintillation Spectrometer ............. 15
5 Cobalt 60 Spectrum Using Two 3 x 3 inch Nal (Tl)Crystals in Sum Coincidence ............. 17
6 Sll Response of RCA-6342A Photomultiplier Tube ...... 22
7 The Sphere with End Flanges in Place ............ 23
8 Carrier for 13/4 inch Crystal Assembly ................... 25
9 Attachments to Crystal Carrier ............. 26
10 Photomultiplier Tube Carrier ....... 28
11 Total Absorption Scintillation Spectrometer .............. 29
12 Cobalt 60 Spectrum from the Crystal ....... 31
13 Cobalt 60 Spectrum from the Anticoincidence Shield ........ 32
14 The Compton Effect ..... 36
v
ABSTRACT
Gamma ray spectrometry is the measurement of the energy dis
tribution of the gamma emission of radioisotopes * Losses of energy
from Compton scattering precludes complete definition of the spectra,
particularly in the lower energy part. An anticoincidence scintilla
tion spectrometer was constructed to reduce the effect of Compton
scattering on spectra. The system consists of a crystal detector
surrounded by a liquid scintillator. The only pulses recorded are
those from the crystal detector which are not in coincidence with
pulses from the liquid detector. Since most scattered photons will
escape from the crystal and be absorbed by the liquid, only those
events resulting in complete energy absorption in the crystal will be
detected thus reducing the Compton portion of the gamma ray spectrum.
This arrangement also helps minimize the natural background contribu
tions to spectra.
INTRODUCTION
The analysis of complex mixtures of radionuclides by gamma ray
spectrometry has become a very common technique„ Definition of the
spectrum is facilitated by obtaining total absorption of the gamma
radiation in the detector. Total absorption results in a spectrum con
sisting wholly of energy peaks from radionuclides present in the mixture
whose intensities are proportional to those of the incident gamma rays.
Total absorption may be precluded by the escape of secondary photons
from the detector. Background also tends to complicate a spectrum but
its effect can be minimized by subtraction.
The escape of gamma photons may be limited by employing a large
detector or by compensation for the effect of their escape. Sodium
iodide crystals with diameters of fourteen inches are available and the
spectra obtained by using them can be expected to reflect nearly total
absorption. Large liquid scintillators have been used extensively for
whole body counting but for routine gamma ray spectrometry their poor
response to low energy radiation limits their usefulness»
Anticoincidence shielding has been found to be very useful in
reducing the intensity of the Compton continuum. The detector is sur
rounded by a scintillator which is connected in anticoincidence with it
so that only pulses representing total absorption in the detector are
counted. Davis, et al., (1956) used a liquid scintillator shield around
a sodium iodide crystal while Perkins, et_ al. 9 (1960) surrounded one
sodium iodide crystal with a sodium iodide crystal and another with a
plastic scintillator. All systems provided significant reductions in
the intensity of the Compton continuum.
An additional solution to the total absorption problem has been
the sum coincidence method which records only coincident events in two
detectors where total absorption occurs. The two events are summed to
gether giving a peak at the summed energy which is satisfactory if it
is known where this peak will appear, JL.jB. , the components of the sample
have been identified.
The construction of a total absorption scintillation spectro
meter will simplify investigative work in neutron activation analysis
and serve as an educational tool. It should provide spectra which are
relatively free of the effects of Compton scattering and background
radiation. The energy peaks should be well resolved. The system must
be versatile enough to present accurately spectra of radioisotopes emit
ting gamma rays at any energy.
THEORY
Gamma Radiation
Gamma radiation is detected by its interaction with matter.
There are three main interactions which occur: photoelectric, Compton
scattering, and pair production. The photoelectric effect occurs when
photons transfer all of their energy to a bound electron of an atom,
usually in the K or L shell, which is in turn ejected with a kinetic
energy equal to the energy of the incident photon less the ionization
potential of the electron. The range of this electron is very short in
most elements and the probability of escape from a scintillator is quite
small. The cross section per atom, t , for photoelectric absorption in
the K shell is given by Kaplan (1962) as:
a x - v W 4 / 2 ( ^ ) 7/2 (1)
where
2<t>o = -y ( - ^ y ) 2 = 6.65 x 10“25cm2 (2)
m c o
2Z is the atomic number of the absorbing material, m e is the rest massoof the electron, hv is the energy of the incident photon and e is the
charge on the electron. (f>o is the cross section for Thomson scattering.
4The Compton effect occurs in an interaction between an atomic
electron and a photon. The electron is separated from the atom and
ultimately absorbed while the photon is scattered from its original
course with a reduced amount of energy. The electron’s energy is the
difference between that of the incident and scattered photon. Since
the scattering is random, recoil electrons over the whole energy range
are produced and, upon their absorption in the scintillator, the Compton
continuum appears. The Compton edge denotes the maximum energy of the
recoil electrons. A detailed treatment of this effect may be found in
the Appendix. The cross section for Compton scattering, , is the sum
of the cross sections for energy transfer to the absorbing material and
the energy in scattered radiation. From Kaplan (1962) :
hole in the negative energy state. This hole constitutes a positron
while the electron in the positive energy state remains an electron. The
interaction occurs in the coulombic field of the nucleus. Disregarding
the small amount of recoil energy of the nucleus, all of the energy of
the incident photon is transferred to the pair of particles in the form
ln(l+2a)]+ ln(l+2a)
where <j> is defined in Equation (2) ando
hv (4)a = 2m c o
Pair production occurs when an electron is raised to a state of9positive energy by a photon of at least 2 m c*- (= 1.02 MeV) leaving a
of their kinetic energies and rest masses. At the end of its range the
positron interacts with an electron producing two annihilation radiation
quanta having energies of 0.511 MeV each. One or both of these photons
may escape or be absorbed in the material through Compton or photoelec
tric processes. The probability for pair production interaction, K, is
normally expressed in units of <t> where
2 2J = JJJ = Z2 x 5.796 x 10~28cm2 (5)
m c o
Z is the atomic number of the absorbing material, e is the charge on the 2electron and m^c is the rest mass of the electron (Kaplan 1962).
Figure 1 shows the regions of dominance for each of the three
effects in sodium iodide and is typical of all matter. The broad range
of the Compton effect indicates that in any spectrum there will be a
continuum.
Background Radiation
Ionizing radiation, produced directly or indirectly by the inter
action of cosmic radiation with the detector, is the fundamental source
of background in counters (Watt and Ramsden 1964). Other sources are
radioisotopes and electronic devices in the vicinity of, or connected to,
the detection system.
Cosmic radiation consists of protons, electrons, neutrons, other
particles and photons. The effects of this radiation upon a scintilla
tion system can best be suppressed by surrounding the detector with a
shield. The most effective shield is one which maximizes photon
Cross
Section
(cm
100
10 -
i H
Total
0.1 Compton
Photoelectric
f Pair Production
0.0110 .01 0.1 10
Energy (MeV)
Figure 1. Absorption Cross Sections for Gamma Radiation of Nal (Tl) .(Data from NBS Circular No. 583, 1957. Reprinted from Harshaw Scintillation Phosphors)
attenuation but limits the resultant production of bremsstrahlung. Such
a shield will readily attenuate particulate radiation.
Scintillation Spectrometry
A scintillator, or phosphor, converts the energy in the course
of the three processes (photoelectric, Compton and pair production) into
visible light. The light excites the photocathode of the photomultiplier
tube, which is optically connected to the scintillator, causing the emis
sion of electrons from it. These electrons are accelerated by the
potential between the cathode and the first dynode of the tube. Upon
striking the first dynode the excess energy of each electron causes the
ejection of more electrons which are accelerated to the second dynode by
the potential between dynodes one and two. This process is repeated for
each of several dynodes until the electrons reach the anode of the tube
and an electrical signal, proportional to the incident photon, leaves the
tube. The output signal is amplified and stored according to pulse
height by a multichannel analyzer.
The scintillation process varies with the materials used. In
the case of activated sodium iodide crystals, the chain of events has
been postulated as the production of electron-hole pairs by interaction
of a gamma photon with the crystal material and the subsequent absorption
of the resultant photoelectron (Birks 1964, pp. 68-93). These pairs
recombine to produce an exciton, which diffuses through the lattice ulti
mately being captured by a luminescence center. This excitation energy
is quickly brought to thermal equilibrium in the lowest excited state 3Pq , the excess energy being dissipated as phonons to the lattice. The
energy from this excited state is then expended in thermal activation,3by capture of phonons, to the level, from which luminescence emis
sion occurs. Luminescence is the emission of light (visible or ultra
violet) with a characteristic spectrum.
The conjugated and aromatic organic molecules have luminescence
associated with them as an inherent molecular property in contrast to
the alkali halides in which luminescence is a property of the crystal
lattice. Luminescence in organics is a result of the electronic struc
ture of the molecules. This property is exhibited in the vapor state,
in liquid and solid solutions, in the crystalline state and to some
extent in the liquid, plastic and glassy states. The structure of
organic molecules is largely determined by the electronic structure of
the carbon atom and the molecules in turn are loosely bound together
and retain their individual identity, electronic structure and lumines
cence. The organic compounds generally used as scintillators include
anthracene, toluene, xylene and trans-s tilbene.
THE TOTAL ABSORPTION PROBLEM
The deviation of gamma ray spectra from the ideal is primarily
a result of Compton scattering. If a scintillation spectrometer can be
constructed to minimize this effect, the spectrum obtained from a par
ticular sample should consist of the energy peaks corresponding to the
energies of the emitted photons. Figure 2 presents spectra for Cobalt
60 obtained with and without the use of an anticoincidence shield in
the detection system.
The primary absorption of gamma rays is an exponential function
of distance which is dependent on energy and the material through which
it passes.
The intensity. I, of monoenergetic gamma radiation at any dis
tance, x, from a point isotropic source is given by:
I = Bl^exp (-yx) (6)
where
I is the initial radiation intensity o
B is the buildup factor
y is the mass attenuation coefficient.
The mass attenuation coefficient is a function of the material
through which the radiation passes and the energy of the radiation.
That portion which is due to the Compton effect accounts for the partial
Coun
ts/s
ec
10
1000
Without Anticoincidence
1.17 MeV1.33 MeV
1002.5 MeV
ComptonContinuum
10 - Backscatter peak
With Anticoincidence
1000800600400200Pulse Height
3 1Figure 2. Cobalt 60 Spectra Using a 4 v x 5 y inch Nal (Tl) WellCrystal. (From R. C. Davis, P. R. Bell, G. G. Kelley and N. H. Lazar, IRE Trans. on Nucl. Sci., NS-3, Nov. 1956)
11transfer of energy to the electron. As the absorber thickness increases,
the number of secondary photons produced builds up and, although many
are absorbed, the number of photons at a particular point in the absorber
is larger than that predicted by use of the mass attenuation coefficient
alone. The buildup factor accounts for this fact.
Large Crystals
The alkali halide crystals are probably the most widely used
scintillators. Their absorption properties are superior to the organic
scintillators because of their higher densities and the higher atomic
numbers of their constituent elements. For example, sodium iodide has3 3a density of 3.76 gm/cm as compared to 0.86 gm/cm for toluene. The
significance of higher atomic numbers lies in the correspondingly higher
photoelectric absorption coefficients. (Sodium 11 and iodine 53 vs
hydrogen 1 and carbon 6.)
The size of a sodium iodide crystal required to obtain 90%
absorption of 3 MeV gamma radiation from a point isotropic source can
be calculated from Equation (6)
Y" = 0.1 = 2.72 exp (0.036)(3.76)(x) = 24 cm or 9.45 in. (7) o
The buildup factor in this case is that for tin whose absorption coeffi
cient closely approximate those of sodium iodide and whose atomic
number is close to that of iodine (Goldstein 1959).
Four pi geometry should be used, jL.je. , the sample should be
completely surrounded by the detector. This is attained by utilizing a
12
cylindrical crystal with a well drilled in it for the source. In the
example, the crystal would have to be about 19 inches in diameter by 19
inches long. The resultant spectra using such a scintillator should
lose a minimum of secondary photons from Compton scattering.
The most frequently used background shield is lead. Four pi
geometry is desirable for the shield as well as detector. Care must be
taken to utilize low noise electronic equipment with the detector because
the shield only protects from external radiation and noise.
Anticoincidence Shielding
The simplicity of a scintillation system such as a properly
shielded large sodium iodide crystal would seem to be ideal for total
absorption work. Use of a smaller crystal with an anticoincidence shield
can provide comparable results. Although the percentage of radiation
absorbed is considerably lower, the distortion caused by Compton scat
tering can be reduced.
The use of an anticoincidence shield has found wide acceptance
in total absorption scintillation spectrometry because it is economically
attainable where a large crystal may not be. The advantage exists of
eliminating unwanted pulses from the spectrum of the sample under inves
tigation. Where lead passively absorbs external radiation, the anticoin
cidence shield detects this radiation and eliminates it from consideration,
in the anticoincidence circuit of the counting equipment. Figure 3 is
a block diagram of such a system. If a photon, no matter what its origin,
enters the shield and interacts with it in any manner so that it is
detected by one of the photomultiplier tubes, a pulse goes to the
13
Photomultiplier Tubes
Photomultiplier Tubes
CrystalDetector
AnticoincidenceCircuit
MultichannelAnalvzer
Scintillator
Figure 3. Block Diagram of Anticoincidence Scintillation Spectrometer.(From W. H. Ellett, "Proc. of Total Absorption Gamma-Ray Spectrometry Symposium,M p. 60, TID 7594 1960)
14
anticoincidence circuit. If there is a time coincident pulse coming
from the principal detector, it is not counted. Only those pulses from
the principal detector which are not in coincidence with pulses coming
from the shield are passed and counted.
The effect of the shield on a spectrum can be evaluated by deter
mining the reduction in the Compton continuum. Equation (6) without the
buildup factor, can be used to calculate the fraction interacting in the
shield.
1 - ~ = exp (-yx) = 1 - e (8)o
where y is the mass attenuation coefficient of the shield and x is its
thickness. The buildup factor is not included because any photon inter
action is effective and total absorption is not necessary. For an
organic shield ten inches thick, 55.8% of 3 MeV gamma radiation which
escapes the crystal will interact in the shield and the Compton continuum
will be reduced that much. The effect will be the same if the organic is
liquid or solid.
Four pi geometry in the shield system provides strong assurance
that secondary photons will interact with the shield resulting in a coin
cident event. A spherical liquid shield appears to be the best all
around solution. Perkins et̂ al., (1960) and Ellett (1960) employed solid
shields in cylindrical configurations and achieved satisfactory results
for their purposes. Davis et al., (1956) used the liquid shield arrange
ment shown in Figure 4. The solution phosphor is xylene, p-terphenyl
and a-NPO. The tank interior surface is a-alumina reflector. The tank
Sheet Iron Tank
Figure 4
PMPMSolutionPhosphor
Source0.005 Aluminum
Solution Phosphor
PM PM
CrystalandPM
PM
An Anticoincidence Scintillation Spectrometer. (From R. C. Davis, P. R. Bell, G. G. Kelley and N. H. Lazar, IRE Trans, on Nucl. Sci., NS-3, Nov. 1956)
16
is 28 inches in diameter and the sodium iodide well crystal is 4 3/4 x
5 1/2 inches» The spectra in Figure 2 were obtained using this scin
tillation spectrometero
Sum Coincidence
The sum coincidence method of total absorption provides another
means of minimizing the Compton portion of the spectra. It is especially
good for the measurement of gamma radiation spectra emitted in cascade
disintegrations, jl.jb. , decay occurs by positron or negatron emission22followed by gamma radiation coincident with annihilation quanta. Na
and Na^ are isotopes which decay in this manner. The gamma rays are
detected in coincidence by two crystals butted end to end and counted
separately. If both counters have the same energy response a sum pulse
which is proportional to the energies absorbed in the two crystals is
sent to a differential discriminator. This component must be adjusted
so that an output pulse appears only when the input signal indicates that
total energy absorption has occurred in the crystals. The only way that
a proper adjustment may be made is if the constituent elements of the
sample being measured are known to be present in it. Figure 5 presents
the results of one such arrangement»
Perkins (1965) describes a coincidence-anticoincidence scintilla
tion spectrometer which seems to optimize the features of both systems.
The shield enables the investigator to obtain a true spectrum of the
sample under examination and the coincidence system permits attainment
of specific total absorption peaks,. For examination of samples with
unknown constituent elements the sum coincidence method does not offer
Coun
ts/m
in/K
eV17
15
10
5
00 1 2
Energy (MeV)
Figure 5. Cobalt 60 Spectrum Using Two 3 x 3 inch Nal (Tl) Crystals inSum Coincidence. (From W. H. Ellett, Proc. of Total Absorption Gamma-Ray Spectrometry Symposium, p. 60, TID 7594 I960)
18
much assistance but for particular work when these elements are known it
is an excellent adjunct to an anticoincidence system.
The best solution to the total absorption problem appears to lie
in using a large size alkali halide well crystal surrounded by an alkali
halide crystal sphere in anticoincidence. This provides best absorption
in the principal detector at any energy and the highest probability for
interaction in the shield. The expense involved in such an undertaking,
however, is prohibitive. The alternative of a large crystal without a
shield is attractive hut again expensive. A smaller crystal in a four
pi organic shield seems to offer something which is attainable. Further,
use of a liquid shield offers the capability of using different sized
crystals with the same shield. This versatility permits the spectro
meter to be used in experiments involving radiations over a wide range
of energies.
SYSTEM DESIGN AND CONSTRUCTION
The primary consideration in the design and construction of any
scintillation spectrometer is to obtain a system with the best possible
resolution. Resolution is a function of the performance of the compo
nents of the system. The variables which contribute most to it are the
emission of light photons by the scintillator, the collection of these
photons by the photocathode, the emission of photoelectrons and their
collection at the first dynode, and the electron multiplication process.
The optical coupling must be complete between scintillator and photo
multiplier tube and a light tight seal must enclose both components to
minimize the loss of visible light photons. The scintillator should be
covered with an efficient diffuse reflector at all points not in con
tact with a photomultiplier tube.
The particular aim in the design of this scintillation spectrom
eter is to minimize the effects of Compton scattering on spectra. In
addition, it would be advantageous to have a portable system for maximum
versatility.
It has been explained that the effectiveness of an anticoinci
dence shield is dependent upon its constituent elements, thickness and
geometry and the energy of the impinging radiation. The presence of
background and Compton counts in spectra from this system will vary
inversely with the probability of interaction in the shield, hence the
material to be used must have the properties necessary to obtain maximum
19
20interaction. The use of any organic liquid for this task immediately
suggests a container large enough to assure a high probability of inter
action because of the low mass attenuation coefficient.
The liquid scintillator chosen for use as the anticoincidence
shield was toluene with p-terphenyl and POPOP (p-Bis(2-5-phenyloxazolyl)
-Benzene)» Toluene is an aromatic solvent which scintillates quite well.
It has good efficiency when used in large volumes because it is highly
transparent. Its disadvantages are its low flash point and high toxicity
which require that extreme caution must be exercised when using it. A
disadvantage which it has in common with other aromatic solvents such as
xylene and trimethylbenzene is that they dissolve conventional polyethy
lene and polypropylene over long periods of time. The latter two also
require caution in their use and their scintillation properties are not
as good as toluene.
Although toluene by itself is an adequate scintillator3 its
efficiency is increased by the addition of p-terphenyl and POPOP. Birks
(1964, p. 295) reports that use of 4 grams of p-terphenyl and 0.1 gram
of POPOP per liter of toluene has been found to be a satisfactory compro
mise between efficiency and material economy. The quick transfer of the
excitation energy in the solvent to the p-terphenyl serves to reduce the
non-radiative dissipation of this energy by quenching in the solvent.
POPOP is added to increase the wavelength of the light so that it more
nearly matches the spectral response of the photomultiplier tube viewing
the liquid scintillator. For tubes with an Sll response a concentration
of 0.1 gram of POPOP per liter of toluene with 5 grams of p-terphenyl
gives a near optimum result.
21The detection of scintillations in the liquid anticoincidence
shield must trigger quick reactions in the photomultiplier tubes so that
the anticoincidence circuit may correctly compare coincident events. If
the liquid is sufficiently transparent, as toluene is, the photomulti
plier tube must be responsive to the incident light to provide a correct
output pulse. The RCA-6342A tube has these characteristics. The antic
ipated light wavelength in the.solution is 4440 angstroms and this tube
has its maximum response at 4400 + 500 angstroms. Figure 6 presents the
response curve for this tube. The transit time from photocathode to
anode is four nanoseconds which is the best for its size.
The efficiency of a liquid scintillator can be reduced by quench
ing due to oxygen dissolved in the solvent. Experiments have shown that
quenching is very significant in toluene. Various methods have been
employed to eliminate the oxygen but the one best suited for this appar
atus consists of bubbling an inert gas through the liquid for about
fifteen minutes. Argon will produce as good results as nitrogen and it
need not be purified before use (Ott jBt _al. , 1955) . Increases in pulse
heights of 20 to 30% have been achieved through this process.
Two aluminum hemispheres, shown in Figure 7, were obtained for
the liquid container. The dimensions are such that with the carrier for
a five inch crystal assembly in place, at least ten inches of liquid
remain for an anticoincidence shield. There is a 74% probability of
interaction in this thickness of organic solvent for 1.17 MeV photons.
The modifications that were made to each hemisphere to accommo
date the crystal carriers are also shown in Figure 7. In both cases
the flange heights are such that their horizontal planes are tangent to
Relative
Sens
itiv
ity
22
Maximum ResponseIOC-
10
40003000 60005000Wave1en g th-Angst roms
Figure 6. Sll Response of RCA-6342A Photomultiplier Tube. (Radio Corporation of America)
ml co
23
■jr Drain PipeGas Pipe
Figure 7. The Sphere with End Flanges in Place.
m|oc
24the sphere at the polar axis thus preserving the spherical configuration
of the tank. The openings are large enough to pass the carriers for
crystal-photomultiplier tube combinations up to five inches in nominal
diameter.
The length of the crystals with their photomultiplier tubes and
preamplifiers caused their carriers to be so long that they became tunnels
passing completely through the sphere. Figure 8 depicts the carrier for
a 1 3/4 inch crystal detector. The assembly is inserted from the bottom
of the tank. For larger sized crystals a separate container with its own
photomultiplier tube could be placed in the vacant space in the carrier
to complete the four pi geometry. In the event that a two crystal coin
cidence arrangement were used, the second assembly would be inserted in
the open end of the carrier. The wall thickness of the carrier is minimal
to reduce radiation absorption. Aluminum has a high mass attenuation
coefficient and any absorption which occurs will result in more counts
in the Compton portion of the spectrum. It is desired to have maximum
absorption in the crystal, but of the photons escaping, the intent is
that there be maximum interaction in the liquid, that is, minimum absorp
tion in the region between the two detectors. There will be a certain
amount of backscatter because of this wall but its thinness should mini
mize the effect. The assembly is fixed to the lower flange by eight
screws at intervals of 45°, Figure 9 presents the fixtures which attach
to the crystal container. The plate, a, is connected to the flange of
the upper hemisphere by eight screws. The container passes through the
center of the plate which serves as a cover for the tank. The tank is
filled with liquid by removal of the plate. A spacer, b, fits in the
25
Figure 8.
m I ooCM
i"ifsZZZZzT
U l x J
x / X
■3 inch Aluminum Tube 0.035 inch Wall Thickness
? 7 7 7 3<
Carrier for 1— inch Crystal Assembly.
<cr
Figure 9. Attachments to Crystal Carrier.
27bottom of the container between the base of the detector assembly and
the retainer cap, c„ Both spacer and cap are hollow so that the power
and signal cables may pass between the preamplifier and the counter.
The cap is fixed to the crystal container by eight screws, The spacer
positions the detector assembly at the center of the sphere.
Figure 10 is a drawing of the photomultiplier tube container.
The small lip is the same thickness as the sphere so that heliarc weld
ing is facilitated. Four flanges have been placed on each hemisphere
at 90° intervals. Initially, only four photomultiplier tubes are being
used, two up and two down. The additional four, when installed, should
provide a significant improvement in the spectra because of the increase
in collection of visible light photons. The face of each photomultiplier
tube will extend into the liquid 1/8 inch to take full advantage of the
field of vision of the photocathode. It is estimated that this field
covers 165° and that the dead space around each tube will amount to 33,25 in . With eight tubes in operation coverage will overlap and the
dead spaces will be eliminated. With only four tubes in place it is
expected that the dead spaces will not be covered even if the lower set
of tubes were to be oriented 90° away from the upper set.
Figure 11 is a partial cutaway of the assembled apparatus, "A"
is the detector assembly while !tBn and "C" are the preamplifiers in the
anticoincidence shield. The lower two photomultiplier tubes and preampli
fiers are not shown since they are 90° away from the upper set. The two
hemispheres as shown are welded together at the center plane by a bead
weld. ;
'4 “20 Tap
iDrill
ra
4Tr̂ loo
H
i>-
TL4r~ vDL Mi—1| 00
2.129 x _ i . 20 Tar
Figure 10. Photomultiplier Tube Carrier.
29
Teflon packing
Teflon packing
Gas PipeDrain Pipe
Teflon packing
Figure 11. Total Absorption Scintillation Spectrometer.
OPERATION
The initial checkout of the assembled scintillation spectrometer
was performed by operating the crystal detector and the anticoincidence
shield separately. This insured that each was operating properly with
respect to the other.
Figure 12 is the Cobalt 60 spectrum obtained by the crystal
detector alone which was used as a basis for comparison with spectra
obtained by the anticoincidence shield. Initially each detector assembly
in the shield was operated individually until common operating conditions
were established for all four. The detectors were then connected in
parallel so that the anticoincidence shield was performing as a single
detector assembly. Figure 13 is the spectrum obtained from the anti-
coincidence shield using the same sample in the same position as for the
spectrum obtained in Figure 12. The poor resolution obtained in the
anticoincidence shield may be attributed to the absorption in the crystal
and the size of the liquid.
It was not possible to employ the anticoincidence shield in its
designed mode of operation. The difficulty appears to be in the elec
tronics of properly matching the output signals from the crystal detec
tor with those from the anticoincidence shield to obtain the desired
effect.
30
31
CM
00
OO vO00 Oi—I i—I
(^0TX) a^nufui/s^unoo Figure 12. Cobalt 60 Spectrum from the Crystal.
Channel
Numb
er
32
o1—4
CN r—I
or—I
c00
00 VO oCM
(£0Tx) a^nujui/s^unoj
Figure 13. Cobalt 60 Spectrum from the Anticoincidence Shield.
Channel
Numb
er
CONCLUSION
This total absorption scintillation spectrometer should demon
strate an excellent capability for unscrambling the spectra of complex
mixtures of radionuclides» Significant reductions in the Compton and
background portions of the gamma spectra simplify the task of identifying
the radionuclides producing the spectra. The system is versatile in that
it can handle varying sized crystals ̂ either singly or in pairs and it
is mobile in that it can be moved about for use in different projects.
With the addition of four more photomultiplier tubes to the anticoin
cidence shield there should be a further improvement in the spectra
obtained. Additional experimentation may be desirable in order to
improve the spectra by using larger photomultiplier tubes or more of
the two inch size. Variations in the solute concentrations in the
anticoincidence shield may also tend to improve the spectra.
Replacement of the aluminum crystal carrier by one of methyl
methacrylate will permit the assembly to be used as a multidimensional
coincidence spectrometer for high energy work rather than just two
dimensional. This change will require a use of different liquid since
toluene attacks methyl methacrylate, Faissner et al. ? (1963) report
that a solvent, Shellsol A, which is not available in this country at
present, has scintillation properties which are nearly equal to those
of toluene. It is safer to handle and lacks the solvent power of toluene
and xylene.33
34The incorporation of a sample transfer system would enlarge
further the operation of the spectrometer. It could then be used for
analysis of elements with very short half lives.
\
APPENDIX
A. Ho Compton (1923) developed the mathematical description of
an effect which results from the scattering of electromagnetic radiation
by matter. He found that when monochromatic X-rays were scattered by a
light element, such as carbon, the scattering radiation fell into two
components, one of the original wavelength and one of a longer wave
length. The difference in wavelength was found to vary directly with
the scattering angle. At an angle of 90° the difference in wavelength
was found to be .0236 x 10 cm. regardless of the wavelength of the
original beam and the scattering material.
Compton assumed that a collision had occurred between a photon
and a free electron in which there was conservation of energy and momen
tum. By quantum theory electromagnetic radiation has energy hv and hvmomentum — c
where-27h is Planck's constant, 6.61 x 10 erg sec
v is the frequency of radiation, and
c is the velocity of light, 2.998 x 10*^ cm/sec.
Figure 14 is a representation of the scattering process. For conservation
of momentum the electron involved in the collision recoils with a momentum
equal to the vector difference between that of the incident and scattered
photon. The reduced momentum of the scattered photon means a lower fre
quency or a longer wavelength than that of the incident photon.
35
36
Scattered PhotonhvMomentum
Incident Photonhv
Momentum =
Recoiling Electron m v
Momentum = — -V T 7
Figure 14. The Compton Effect.
For conservation of energy
hv = hv + m c' o o - 1 (1)
where:
is the frequency of the incident radiation
v is that of the scattered radiation
v is the recoil velocity of the electron,-27mo is mass of the electron, 0.9107 x 10 gram.
and.
c is the velocity of light.
For conservation of momentum there are two equations for the two compon
ents :
hv , m vo hv . . o x-component: --- = — cos® + ,, • -• -i— - cosic c V I W
(2)
hv moVy-component: 0 = — sind) - sinB (3)
where <p is the scattering angle of the photon and 0 is the recoil angle
of the electron.
Let 0 = “c
then these three equations may now be solved for v, v and 0 for any
particular scattering angle, The respective wavelengths are
38
so Equations (2) and (3) become
, , m 8cT T cos* = --7T- COS6 (4)xo x
m 8c— slncf) = 7- -rr sin0 (5)x V i - s 2
Squaring these and adding
9 9 9 2*2 2 _ 2 2h h 2h cos* mo 8 C o c 2 2 f n-4- — — - :— :— - ---- = — - m c (o)X 2 X2 XoX 1-62 1-B2 °
Also Equation (1) becomes
, , m e— - — + m c = - °— (7)X X o ¥
Vl-B2
and squaring it
75 + 71_ rr + 2™0ch(r" - b + mo2c2 “ TTI (8)A A O O 1—P
Y Y (cos<f>-l) + 2m^ch(^- - ^) = 0 o o
or
AX = X -X = --- (1-cos4>)o m e o(9)
39
It can be seen that the shift in wavelength is dependent only upon the
scattering angle of the radiation since " • is constant.m c o
h = 0.0242 x 10 8 cmm c oso
AX = 0.0242 (l-cos4>) angstroms (10)
The kinetic energv of the recoil electron is
T = hv - hv o
hvh^(l-cos$)^§Y (ID
or, if
a
hvH — ‘C 1-cos 4))
m c o
hvo2m c o
a(l-cos^)hv l+a( 1-cos <{))T = -r— TT --- (12)
This will vary from <t> = 0°, 9 - 90°
where T = 0 to a maximum
when (J> = 180°, 6 = 0°
40This energy denotes the Compton edge. The corresponding energy of the
scattered photon is
hvhv = i^a-cos*) (14)
Some photons are scattered back by the housing of the scintil
lator and photomultiplier tube. The peak of the distribution of the
resultant pulses in the spectrum is the back scatter peak and corres
ponds to the energy of photons scattered at an angle of 180°,
hvEbs - iTit <15>
by Equation (14).
LIST OF REFERENCES
Birks, J» B.5 The Theory and Practice of Scintillation Counting, NewYork: The Macmillan Company, (1964).
Compton, Arthur H. 5 Phys» Rev. 9 21.) 483 (1923) .
Davis, R. C., P. R. Bell, G. G» Kelley and N, H. Lazar, IRE Trans., NS-3, (November 1956).
Ellett, W. H., Proc- of the Total Absorption Gamma-Ray Spectrometry Symposium, TIP 7594, (1960), 60-70.
Faissner, H., F. Ferrero, A. Ghani and M. Reinharz, Nucleonics, 21,(February 1963), 50.
Goldstein, Herbert, Fundamental Aspects of Reactor Shielding, Reading Addison-Wesley Publishing Company, Inc., (1959), 221.
■Kaplan, Irving, Nuclear Physics, 2d ed., Reading: Addison-WesleyPublishing Company, Inc., (1962), Chap. 15.
Ott, Donald.G., F. Newton Hayes, Jay E. Hammel and John F. Kephart, Nucleonics, 13, (May 1955), 62.
Perkins, R. W., J. M. Nielson and R. N. Diebel, Proc. of the TotalAbsorption Gamma-Ray Spectrometry Symposium, TIP 7594, (1960) 48-59.
Perkins, R. W. , Nucl. Instr. & Meth. , 3_3? 71, (1965)
Watt, D. E« and D. Ramsden. High Sensitivity Counting Techniques,New York: The Macmillan Company, (1964).