GAMMA RAY SHIELDING - IAEA

16
PINSTECH/HP-1G GAMMA RAY SHIELDING ANWAR AL1 M. A. MUBARAK HEALTH PHYSICS DIVISION PAKISTAN INSTITUTE OF NUCLEAR SCIENCE I TECHNOLOGY ' ISLAMABAD 1971 We regret that some of the pages in the microfiche copy of this report may not be up to the proper legibility standards, even though the bsst possible copy was used for preparing the master fiche.

Transcript of GAMMA RAY SHIELDING - IAEA

Page 1: GAMMA RAY SHIELDING - IAEA

PINSTECH/HP-1G

GAMMA RAY SHIELDING

ANWAR AL1

M. A. MUBARAK

HEALTH PHYSICS DIVISION

PAKISTAN INSTITUTE OF NUCLEAR SCIENCE I TECHNOLOGY ' ISLAMABAD

1971

We regret that some of the pages in the microfiche copy of this report may not be up to the proper legibility standards, even though the bsst possible copy was used for preparing the master fiche.

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PHISTBCH/HP-10

GJ&m RAY SHIELDING

ABWAR A U M* A. MUBARAK

HSALE2 raYSICS DIVISION FAKISfAIT IITSflOTS OF ffiJCLEAR SCIENCE AND ^C^TCLCGr

ISLAMABAD 1 9 7 0

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?Ii

GA*5KA RAY SHIELDING

Anwar Ali Id* A* Mubarak

ABSTRACT

This report discusses the shielding properties of common shielding materials such as lead, iron, concrete and water and is expected to be helpful in designing shields and containers for safe handling, storage and transport of gamma emitting radioactive materials* Maximum energy of the photons considered is 3 MeV.

Health Physics Division Pakistan Institute of Nuclear Science and Technology

ISLAMABAD 1970

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CONTENTS

'age

Introduction .. •• •• • • •• .. • • •• • • • • •• 1 Shielding Parameters • • ?.

£•1 Unit of Re-diction Dose-Roentgen •• . . •• ••• 2 2.2 Conversion Factor K k

2*3 Linear and Mass Absorption Coefficients•• ... 5 2.4 Build-up Factor .. .. • • • • 7

Shielding for Uon-Foint(Extended) sources • •• • 3 3*1 Line Sources •• •• •• •• •• •• .• •• •• «•• 8 3.2 Plane Disc source •• •• •• •• •• •• • • • ... 10

Transmission of Gasaaa Radiation through Lsad, Iron,Concrete and Water. •• •• •• •• •• • • 11

Tr&nsoission of Gacsma Rays from some specific Isotopes. •• •• •• •• •• •• •• .. • » •• 12

Tables • . . . . . 13,

References •• •• • • •• •• .. •» .. •• •• 15

Figures.

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1.INTRODUCTION Gorjcia radiations are electromagnetic in

nature and as srca possess greater power of penetration than other types of nuclear radiations(except neutrons). For example thicknesses of 0*025 meters and l6«5 meters of air are sufficient to stop k KeV alpha and k KeY beta particles respectively, but a thickness of 190 meters of air is required to reduce the intensity of k MeY gamma rays by a factor of 2,

~«/hen gamma radiations pass through matter their intansity is decreased due to interactions such as photo-electric effect, compton effect, pair production and photo-nuclear reactions* Use of matter as a shield to reduce the intensity of ganaa radiation is known as shielding* The effectiveness of a shield depends on the energy of the radiations and on the type cf the shielding material. The higher the atomic number and the density cf the shielding material the more effective it is in reducing the intensity of gamma radiations* This report discus ejs th& shielding properties of common shielding materials such as leadf iron, concrete and water and is expected to be helpful in designing shields and containers for safe handling, storage and transport of gacisia emitting radioactive materials. Maximum energy of the photons considered is 5 MeY.

-1-

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2.SHI3LPXNG PAR/JESTERS In the case of a point source tho usual

expression for dose rate through a shield is given as

A.5. IS* ?

/ ,

where !>• • ' ' dose rate in roent-;ona per hour at a distance d from the sourcj.

X ' a conversion factor equal to the dose rate in roentgens per hour at a distance of 1 cm, from a point source of 1 mi Hi-curie.

S — ~ _ _ — strength of the point source of ga Kie rays in milli curies*

• .. B — — — — dose build-up factor. « — •'•• linear absorption coefficient of the

shielding material in cm • x -,,., , ,„. thiclsnesB of the shield in cm.

The parameters mentioned above are discussed in some detail in the following paragraphs. 2.1. BEit of Radiation Jose - Roentgen

f.

H* might he expected, it is found that the extent of radiation-induced biologic&l damage depends on the *»ergy liberated in the tissue in .the form of ionization. ,$mm types of damages increase nor* or less linearly

,h

" ** ' liL J^ttSUi ';% . ^^K,^,i^ ^^M-'-M^h^^^-^:.:-^^^^^ M->.I>.-, -*...;C*

J»JJ . i i i i im j iMww—wa—aB»wwWW

with the quantity of lonisation, suggesting that the process ft* of a "Target" type, and that the damage, once caused, Is permanent; for other effects the body is provided with a repair mechanism which can prevent to a considerable extent the appearance of any symptoms until a certain threshold dose-rate 4s reached* The damaging effect on the org4 iism as a whole increase* roughly linearly with increasing ionization. ?or this re&aonf the amount of X or ganina radiation is usually measured in terras of a unit quantity which will liberate a standard amount of ionization in a standard substance such as air. Since equal masses of air and tissue absorb X and gamma rays with about equal effectiveness, a given amount of radiation, measured in this way, corresponds approximately to a particular amount of damage, irrespective of the quantum ^n^rgy of the radiation. This unit can be given a dual usggo, and can be used both as a measure of dosage and of quantity of radiations. The unit defined in this way is called "Roentgen" (2). It is defined as*The quantity of X - or gamma radiation such that the associated corpuscular emission per 0.001293 grams of air (one cubic centimetre of air at N.T.P.) produces, In air, ions carrying one electrostatic unit quantity of electricity of either

.~3r* **//$ *N,

X- >

»4Sfe .-ft' ,t$0 *r- 'L "V-* ' '-w4«< 1&L*ij>.**-™*tr**>" .

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2*2*Conversion Factor Z

As defined earlier9 this is equal to the dose rate in roentgens per hour at a distance of 1 cm* frosr a point source of 1 nilli-curie. It will depend on the number of pftotons emitted frost the source per disintegration, the energy of these photons and their mass absorption coefficient in air* Figure (l) give* the linear absorption coefficients in air of plotons of various energies (3).

The gates flux (number of photons/cm* -Sec.) at a distance of 1 ecu from a point source whose strength is one millicurie is given by

« |jjr ^ n i ?notong/cn8*sec (2)

where N c Total number of photons emitted from the source per disintegration

and n. » the number of photon* of energy 2. emitted per disintegration*

The energy absorbed in a cubic centimetre of air due to photons of energy B ± (KeV) will be

•' tl-fS/ 1!)^ MeV/Se©. which foreman values of jn ± will be mqm^L to

*t/*i*l MeV/Sec.

Thus the energy absorbed in a cubic centimetre of air at a distance of 1 cm from a point source of 1 mc will be

s = W^iA*! KeV- (3)

The energy required to produce one ion pair in air is 3k eV(4) and the charge of an electron is ^*SxlG~ c.e.u., hence,

one Roentgen (r) e - \k xlO* KeV -<4>

Thus with the help of equation (3)« the dose r&te at a dist&nce of 1 ess' from a point source of i milli-curie comes out to be

then

£ ;,ffi.8xio3

fcrrx34 *>i/i . E r/Sec•

4l»5 JP n i / * i B 4 r / s e c .

1*49x10' £ n A >»4 *£ r/hour -(5)

If K^ corresponds to the photon of energy B.

X . 4 ,>* Uk9k x 10* *£fi± » 4 r/hour (6)

re*» Equation (6) i s presented graphically in Figure 2 ,

and values of K for various radioactive isotopes are

presented alongwith the ir h a l f - l i v e s in Table I .

a ' « • ^ j ;' ,4

li3U» **f

'jais

>?•*£

/ 'k« fM

i&Mfek.& .fflBET-A » K * t ' / . . -r jf " ^iitr

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2»3» Linear and Masa Absorption Coefficients

The probability that a photon, in traversing s.

slab of material, *ril! be affected by an interaction such as p^ir production, compton scattering or photo-electric effect is most simply described in terns of a cross-section for that interaction*

5 Assume that 0 photons/cm -sec. are normally

incident on a slab of material in which there are H atoas/cfi. Let 0 (x) be the flux of photons at depth x which^have not suffered any collision or interaction i2itheir passage through the slab. Let the probability that a photon, in traversing a further thickness dx, suffers a collision of type i, be dp ±| and assuae, for the moment that no other type of collision is possible. Then f the cross-section/ atom for the process is defined by the equation:

d ? i m N <?j(ixB 12 -

On integrating, the uncollided flux 0 <x) emerging through a slab of thickness x is found to be

Zf more than one process is involved <£~ must be replaced by the sum of the component cross-sections .dTl x«

tot Ths total cross-section depends markedly on both the atonic number of the absorber &&& on the photon energy*

iviBtfv

N£Tt t is known as linear absorption Co-efficient of ths material. N£T .fp is known as mass absorption Co-efficient of the materialywhere C is tho density of the material.

3.km Build-up Factor The exponential law for the attenuation of gacaa

radiations in a material is

0(x) * jQ Z/1* (7)

where 0 O is the original flux of photons, 0(x) is

the flux after traversing a thickness x of the material and n is the linear absorption Co-efficient for this material.

In this equation it i3 assumed that the partict:l4.r photon involved in a reaction such as photoelectric effect, compton effect or pair production in the material is completely eliminated and is not seen by a detector put across the shielding material, but it is true only in the case of narrow beam geometries.

In the case of broad beams of radiation, howovar, the secondary radiations resulting from the interaction of primary photons in the material have every possibility to pass through the shield and thus the photon flux (and therefore the radiation doss) meroi* the shield will be greater than that calculated from equation %• In the

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case of broad beans the e:. (7) will be nodified to 0 a 30o e/^ where 2 is known as build up factor.

3. SHI3LDINS FOR IICN-FQIKT (SXTiSHPSD) S0U3CSS The shielding for point sources of gamma

radiations is discussed in the earlier sections of this report. In actual practice, hc7revcr, the radiation sources are nev^r point sources.

It is a valid approximation to consider a source to be a point source if its dimensions are very snail compared with the distance froa the source at which the dose is required. In other words a source nay be considsred to be a point source if the angle subtended by it at the point of interest is very small. If this is not the case, then certain corrections have to be applied to the dose rates obtained after assuming the source to be a point source. These corrections are discussed for two coaion and simple cases in the following sections.

3»1» Line Sources Consider a line source A3 Pig (k) whose

strength per unit length is S . The contribution of a small element of length dl to the dose rate at a point P across a shield of

-8-

thickness x is given by K.S.

dO = 1. dl B e/ 1* Sec 6

1

Now r = d.Sec 6 and dl = d Sec 6*d6 Thus

dD s.s;

s.Z/* S e c * \d e The lidits of 6 are 0 to &*, and 0 to 6 ? t

therefore the dose-rate at point ? due to the line source A3 will be

I o

6>. 1

1 K.Sj.B. ^IQ^/*-*•) rj-CS^^

flow if the point P lies on the right bisector of the line A31 then

1 2 . 0

and D d

I f the length o f the source i s 21 , %hentiie

s trength of the source S » S„ x 2p and £"m d Tan 0*

Thus D m K t | f B ; F' <^ixf # ) . >W

,,m

Z^^..*/™. 7 (yox, 9)

«*$•«

• /? '£"' • '" ' .A' :*«**. v . : » . , , 1 : . . '

•tosS

;i»^^^^'.^i ; »,,, „ w* , ^ * ^ « * | f e ^ ^ ^ V '•<&* j&afc

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If 6 were small, the lino source could be considered to be a point sourcs and th^ dose rate would have been

D a *** I3*» e / ^ (9) • d?'

Dividing equation (3) by (S/» the correction factor for line sources of radiation cones out to be a function of 6 and nx and can be calculated* Sone value of this correction factor for various values of yux and %

are presented in Table 2* '* • 3*2« Plane Disc Source

Consider a plane disc source of radius R ifhose strength per unit area is S.. The contribution of a small

a element of area ids m r dr.ot0) at a point P situated on a line drawn perpendicalar to the plane of the source from its centre -will be

X.S tr.dr, d0. „ A ' d D = « L 3.5 /« Sec 6

( r .• d > ITow r = d tan ©, therefore dr s d Sec* $• d0*

Thus dO * *.V». d0' T*n*'*f* S e C 6« d e' Integrating thia equation with liaits of 0 beinc

0 to 2Xt and that of 8 being 0 to % where San « 0 » j-.

•10-

we get D = 27rK.s a. S.f/r^x)-F^ J t^^1

Now the total strength of the source S = CT'.r \Sa .2 m 2, es Tfd .Tan'©0.Sa.

Thus

s.s.^- _-/<* d 2 ' € /6**.«0

Now if the disc was considered to be a point source, th3 dose rata at the -goxnt P Would have been

D * £«f*2*.. £ (it) .: d 2

Dividing equation (lQ)'by (ii) the correction factor for a plane disc source of radiation coaes out to be a function of jax and 0O and can be calculated* Some value* of this correction factor for various values of JOX and 0O are presented in Table %,

TRAIISKIgSIOW OW W^ J^I&XOK. .TX*3V&1 t&*i> IRON. gjjJTfe Ii> ttstik.—"^————* «—~*

The equations discussed in the previous sections were used to calculate the attenuation of gaoraa radiation at various energies in various thicknesees of coaaon

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coaaacTioH FACTOR C I ) FOR v;itxou5 V^LUSS OF ax sdio e K 3

D = — ^ i ?1 d

(e/ )

LIII3.30URC3;(at•ri&st angle t > ii&e "joining obsorv^r

Centre of source>

© = 'j?. an^le subtended by l i n e source aeaourycL

obcervar. ( n ) ' • e

5° 10'

30'

• i.OCi i.OCi ! i.001 ? * A~- * * * ^ o I 1,003

1.010

1.103

l .oci * i.ooi j i .ooi \ i.oc?, - < i »

i * • y i.OOfe t i . 0 9 1.016 l 1.036 1.Q16

1*157

1.036

1.37&

1.067 I i . l^S

I.696 ".37-

TA3L5 IIP; 3 (1 ) • . . •

PIgC 30URC3;n(ia plane, aoraal to l i n e jo in ing centre of

source -and observer)

8 as % vert©:: asagie o£ cone subtended by source -.$ observer. /7? \

•to'

30*

idosO

1.00

1.01

1.02

JU3CB1 1UB»5» yPUCsll J? MX*%5

1.00

1.01

1.02

1.00

1.01

1.00 1 • 1.00

A . 30..

j 1.05

i i £ 5

1.04

1.1s

2.5V , fe.36

1.0s

1.20

-14.

RBP3R3NC3S

1* Rockwell 111, T.,(3d.), "Reactor Shielding Design lianual" , D. Van Most rand Coop any, Inc., Princeton, New Jersey, 1956.

2. Price, 3.T., et el., "Radiation Shielding", Pergammon Press, 1957*

3. Radiological Health Handbook, PE l£i73fc R, U.S. Deptt#of Health,Sducntion & Welfare, Dlv. of Radiological Health, Yashins ton 25, 3.C. Sept. I960.

km 3acc, 3.K.t Alexander, I.,"Fundamentals of n RadiobXola€3^ Pergaomon. Press, 1961. 5. 3beling, D.R., "Some Design Data for Gaeuaa Shielding

in N.S.-J., "AASC/3.11., Dec, 1957-6. 51atz, H.(Ed„), "Radiation Hygiene Handbook,

l!cGraw Hill 3ook Company, Inc.,New York, 1959* 7. 2vans, Robly D. "The atomic Nucleus**, McGraw Hill

Sook Company, Inc., New fork, 1967. p.(722).

*fifc\

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^JW^'ll^uitl^WW".' »lil«M!'ll'l.' "—*—

lU t i iiiiiiiiiiiiiM -•m,iiiirin Uifciii ii inrrmwii mmmmmmm

-*,-.

LINEAR ABSORPTION COEFFICIENT OF PHOTONS IN AIR (COMPOSITION OF AIR TAKEN AS 7t74fe,2f/?2 M.A AJ Z(fc) <

1.5 2.0 -^PHOTON ENERGY (MtV)

•'4

i I

34

1 UliHlWiHilim

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Kin IUUJ iK'n. imjtgsfmmmfnm"

PINSTECH /HfMO

H

i t ,

, ' i

!•* wt ^fesfA 1

PtNSTfiCH/HP-lQ

LINE SOURCE (FIG* 3 )

PLANE DISC SOURCE(FIG.O

• f:

* • • /

. • * . „ • » . . „4,;f. ,. ,J . , . / » ,

V;' ! *; I A

*

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- 4 m r> x «•» I ?

tan iiiikMmmm*mmmm

TRANSMISSION

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PINSTECH/ HP-M

TRANSMISSION OF GAMMA RADIATION WITH OOSE BUILD-UP IN

LEAD FOR POINT ISOTROPIC SOURCE

AND PLANE SHELD.

THICKNESS OF SHIELD CENTIMETERS

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PINSTECH/HP-10

TRANSMISSION OF GAMMA RADWION WITH DOSE BUILD-UP IN

CONCRETE FOR POINT ISOTROPIC SOURCE

AND PLANE SHIELD

*> 1S 20 25 30 35 40 45

THICKNESS OF SHIELD-CENTIMETERS 50 55 GO 65 TO 75

PlfrURff-f?)

•*«M!PH|MM*I

PINSIECH/HP-K)

in UJ »~

ui

UJ

X «/> u. o

to

o X

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T*Kif*rfr'.? ••','.' "Life' - :,' '.0. •ijflaig." ' s ALji'^gstLiU'i JiukUiiBMU? ia«*«**vS^W,WWi«M!WSm,®«-i:I3 >i | l |»IB| i l l^'4i i«Wi. . lM. 1,11 l|ilH III