the design, construction, and performance of a · 13. curves of magnetic fiel d vs. coil spacing 31...
TRANSCRIPT
THE DESIGN, CONSTRUCTION, AND PERFORMANCE OF A
i1AGNETIC FOCUSING, SEMI-CIRCULAR, LOW ENERGY
BETA-RAY SPECTROMETER
By
Herbert E. Henrikson
Special Technical Report No. 24
Prepared under Contract No. AT(04-3)-63 with the
UNITED ST.h.TES ATOMIC ENERGY COHMISSION
Jesse i<T.M. DuNond, Contract Supervisor
Calif ornia :nstitute of Technology
Pasada~a, California
October - 1956
ACK NOWLEDGM ENTS
The author wishes to acknowledge the important contributions of
Dr. Pierre ?1armier (now at Physikalisches Institut der E. T. H., Zurich,
Switzerland) in the early stages of the design of the spectrometer.
The concept, design, and construction of the field regulator was
by Dr. Joseph }furray (now at the Radiation Laboratory, University of
California, Berkeley, California) .
The experimental work of Dr. Felix Boehm provided the performance
curves reproduced in this report.
The skillful machine work of Alfred Doering is greatly
appreciated.
ii
I.
II.
III.
TABLE OF CONTENTS
Resume • . . . . . . . . . . . . . . . . Detailed description of the semi- circular
spectrometer and i ts construction ••••••
A. Main field coils - construction and specifications . • . . . . . . . •
B. Current re~~ator . • . . . • . . c. Compensating coils for earth ' s
magnetic field • . . . . D. Spectrometer chamber
l. Source •
Page
1
4
4 9
13 15 15
2 . Geiger counter • • • • 18
3. I nstallation of the spectroMeter chamber • • • • • • • • 18
E. Vacuum system and counter filling system • 20
F. Detecting and recording system • • • • • • 23
Performance curves • • • • •
A. :1ediu.11 er.ergy spectrum of an Yb169 source • .
B. Lm-v energy spectrum of Tm169 follovTing
Yb169 decay and Lu175 following ~75 decay • • • • • • •
C. Low energy spectrum of Tm169 following
24 25
26
Er169 decay • • • • • • • • 27
D. L- Auger in Ft and Os spectrum from
I r 192 decay • • • • • • • • • • . . 28
Appendix ... • • • • . . • • . . . • • • • • • . . • • 29
Hagnetic field study • • • • • 29
Circuit diagrams for current regul ator ••• 35, 36
iii
FIGURES
No . Page
1 . Photographic view of complete spectrometer assembly 2
2. Main magnetic field coils 5
3. Cross- section of main field coils 8
4. Current regulator 10
5. Photographic viel·r of open spectrometer char1ber 16
6 . Source holder 17
7. G. H. counter 19
8. Schenatic diagram cf vacuum and counter filling system 21
9· Medium energy spectrum of an Yb169 source 25
10. A. Low energy beta- spectrum of Tm169 following
Yb169 decay 26
B. Lul75 L- Auger spectrum following ~75 decay 26
11. Low energy spectrum of Tm169 f ollowing Er169 decay 27
12 . 1-Auger in Pt ~illd Cs spectrum from Ir192 decay 28
13 . Curves of magnetic fi el d vs. coil spacing 31
14. Curve of coil spacing vs . radius of homogeneous field 32
15. Cross-section of nagnetic field distribution in the region of the electron trajectories 33
16 . Second order focusing 34
17 . Control chassis and interconnect5.ons for current regulator 35
18 . Pm·rer chassis for c•1rrent regulator 36
iv
I Resume
THE DESIGN, CONSTRUCTION, AND PERFORYJ.ANCE OF A
l1AGNETIC FOCUSING, SEMI- CIRCULAR, LOti ENERGY
BETA- RAY SPECTROi1ETER
A semi-circular beta- ray spectrometer (Fig. 1) has been con
structed for operation between 2 and 120 kev electron energy. This
instrument ,,ras designed to suppl ement the rL'1g- focusing beta-ray spec
trometer1 whose lower linut is approxinately 25 kev. The 180°
spectrometer has an electron traj ectory radius of 12 em. The field is
produced by t wo iron free coils spaced to give a nearly homogeneous
field (Hith some second order focusing) in the region of the electron
trajectories . The field current is su~plied by a one br motor- generator
set . Stabilization is obtained to 2 parts in 10, 000 with a rotating
electro- mechanical unit and an electronic servo system. Source and
Geiger counter windoH d:'....""l.e~sions for a standard resolution of 0 . 8% are
0 .1 em x 4 em. \hth a 10 ~/cm2 formvar windovT, transmission is assured
dovrn to 2 kev electron energy. A recording potentiometer traces the
counting rate vs . electron energy. Several examples of chart recordings
are reproduced to illustrat e the performance of the semi- circular beta
ray spectrometer.
The instrument assembly is shmm in Fig. 1 . The spectrometer
proper is shown in the foreground. The framework is welded aluminum 11T"
section, set on four leveling screws . Nonferrous materials have been
used throughout to avoid field distortions . ~he nearest iron is in the
diffusion pump (9) close to the floor . The s~ectrometer chamber, (1) ,
is located synnnetrically between t.r.e tHo main field coils , (2) . Sur
rounding the assembly are the coils, (3), 1·1hich cancel the earth's
magnetic field. The source holder, (4), and Geiger counter, (5) , are
clamped to the front of the chamber . The counter gas ballast chamber ,
(6), is below the geiger counter and is connected to the filling
1 An Axial-Focusing Magnetic Beta-Ray Spectrometer, by J .H . M.DuHond et al .
-2-
Fig. l. Low energy magnetic beta-ray spectrometer showing: (1) spectrometer chamber, (2) mainfieldcoils, (3) earth 1 sfield compensating coils, (4) source holder, (5) G. M. Counter, (6) G. M. counter filling gas ballast chamber , ( 7) G. M. counter filling system, ( 8) main clapper valve, (9) diffusion pump, ( 10) current regulator, ( 11) generator field power supply, ( 12) control panel (M. G. set, vacuum pumps, etc.), ( 13) current regulator control chassis, ( 14) power supply for compensating coils, ( 15) vacuum gauge, (16) scaler, (17) counting rate meter, (18) cathode follower, ( 19) recording potentiometer.
~-
system,(7). The main clapper valve, (B), is closed to allow the spec
trometer to be opened to the atmosphere while inserting a source or
replacing the counter >vindow. The diffusion pump, (9), is below the
main valve and is connected by rubber hose and brass tubing to the fore
pump located in a separate room.
The main field is controlled by the current regulator, (10),
seen to the right of the spectrometer. The motor-generator set supplying
current to the main coils is located in a separate room. To the extreme
left of the spectrometer is the rack containing the power supply, (11),
for the field windings of t he de generat or. Above that is the control
panel, (12) , for the vacuum p~~ps and the motor-generator . Next is the
control chassis, (13) , for the current ~eg~lator and the power supply,
(14), for the earth's field compensation coils. The vacuum gauge, (15),
is of the cold cathode ionization type. The decade scaler, (16), and the
counting rate meter , (17), are connected through the cathode follower ,
(18), to the Geiger counter . The counting rate is recorded on the strip
chart recorder, (19) .
The t wo m&L~ magnetic field coils are connected in series
for the lower hal: of the spectrometer range (2 kev to 50 kev) and are
switched to parall el fo~ t~e upper half (50 kev to 120 kev) . Except
for this switching opera~ion t he spectrometer, once started, operates
semi-automat ically, shutting down at either end of the range.
The ultimate calibration of the 180° spectrometer depends
on the energy measurements of the curved-crystal gamma-ray spectrometer.
II Detailed Description of the Spectrometer and its Construction
A. Main Field Coils -- Construction and 3>ecifications
In the prel~tnary design of the 180° spectrometer the field
1-ras to be provided by a pair of Helmholtz coils 68 em in diameter and
spaced 34 em apart . This produces a comparatively homogeneous field in
the central region. At the central electron trajectory, (r = 12 em),
the gradient of the field would be o.S% per em. At the widest portion
of the electron beam (2 em) the variation 1-.rould be 1%. Calculations
indicated that the homogeneity in the region of the trajectories could
be improved by decreasing the distance between the V.-10 coils . It was
found that for a spacing of 29 em ( .8S x me~! coil radius) the variation
in magnetic field, at radius 12 em, was 1 part in 1000. This gradient
is of the proper sign to contribute to second order focusing. A de
tailed discussion of the field distribution is given in the Appendix.
To achieve the desired field distribution, each turn of wire
in the upper. coil snould have a matching turn in the lower coil of the
same radius, separated o~r . 8S time their radius . To approximate this
condition each coil is ~-round ui th a cross section of .85 inches by
3.86 inches and the l ong dimension lies along t he generators of a cone
as shown in Fig . 2. The specifications for the main field coils are
given in Table I .
The internal surface of each cast brass coil form was
machined to the same dimensions . Each £'om was lined with 20 mil
fish paper. The winding was done on a large turntable with provision
for maintaining a uniform ~·rire tension. Each layer consists of 22 turns.
To maintain uniform winding, strips of lO mil fishpaper were laid in
every fifth layer. The completed Ninding consists of 91 layers .
Experiments with a model indicated that sufficient cooling
could be achieved by filling the coil form with transformer oil and
passing water through one ~urn of S/16 inch diameter copper tubing
soldered to the inside diameter of the coil form.
rc= coil radius (34cm.)
re= electron trajectory z radius ( 12 em.)
L = co i I spacing (2 9 c m) l r c
~-------------------~-~~ ~ ~
cast brass coil forms ~[---___ I /
'lc: •• __ .../-"'_
~
~ ~ 3.865-A I > ~ inches\ <.
\¢? ~ ~5 inch
L
~
Fig. 2. Cross-section of main magnetic field coils. To achieve maximum homogeneity at the radius of the electron trajectory, (r ). the coil spacing, (L). is fixed at 0. 85 times the coil radius, (r ) . e
c
I V\
I
-6-
TABLE I . SPECIFICATIOKS OF THE MAIN FIELD COILS AND PO:JER SUPPLY
Power Supply
Current Re~1lator
Main Field Coils
Hire size
General Electric r·iotor Genera tor Set
Motor 2 HP, 220 volts , AC 3 ¢ induction tne
Geaerator 1 ~1, 250 volts , 4 a~eres full load (shunt field connected to current regulator)
Rotating electrcmechapical servo system
Current staoility - - 2 parts in 10,000
#19 copper wire (formvar coated)
Number of turns (each) 2000
Resistar.ce of each coil
Insulation
Cross section of each coil
Coil form
Cooling
Field strength (pair)
Total oil expansion (each)
Temperature rise (max .)
113 . 4 ohms at 26° C
heavy formvar coating and fishpaper
.855 inch x 3.865 inches
cast brass (iron free)
oil filled, water cooled form
0 to 120 Gauss
-7-
To seal tte outer edge of each form two cast brass rings
Here machined with 110 11 ring grooves (Fig. 3) and clamped in place . A
l/2 inch x l/2 inch groove w~s r.achined in this outer ring to provide the
coil form for the earth's f~eld compensation discussed in Section II, c. A flexible bellows provides for the expansion of the oil, since the sys
tem must be closed, to prevent moisture from entering the windings . The
two coil leads are brought o~t to terr.Jnal blocks as shown.
The completed coil assembly was evacuated through the pumping
port for a sufficient period to insure the elL~ination of air and mois
ture. Current was passed th:'ough the vrindings to aid in the out- gassing
process . The transfo~ner oil Has out gassed in a separate vacuum chamber
to elininate air bubbles . The evacuated coil \·Tas then impregnated Hi th
the treated oil through the oil filling hole and the holes were sealed.
The coils iiere mounted on their adjustable supports as shmm
in Fig. l. The loi·Ter coil \vas leveled with a precision level in tHo
directions and centered with respect to a fine plumb line suspended from
the top of the main frame . The upper coil Has spaced by the use of an
indicator mounted on a rod 1-rith one spherical end. The tHo coils were
lined up axially by the use of a plumb line held against the inside
diameter of the upper coil at seve~al places .
wa
ter
be
llow
s sh
ield
\.
/ ..
coo
ling
tu
be
oil
. e
xpa
nsi
on
ch
am
be
r
term
ina
l b
lock
\
oil
fillin
g
hole
\ e
art
hs
fie
ld
com
pe
nsa
ting
co
il --
ma
in
fie
ld
win
din
gs
Fig
. 3
. C
ross-s
ecti
on
of
main
mag
neti
c f
ield
co
il.
I 0
>
I
- 9-
B. Current Regulator
A direct neasurement of the magnetic field (0 to 120 gauss)
is very difficult over the entire r~~ge . The proton resonance method is
practical dovm to approxinately 50 gauss . Below this value the requisite
volume of the proton resonance ~~~le becomes prohibitively large . This
range (0 to 50 gauss) represents, in the present spectrometer, the elec
tron energy region (0 to 65 kev) of greatest interest in the planned
research program.
An electromechanical rotating unit vias found to be most ade
quate for the present pur? ose . This rotating unit operates as a current
regQlator rather than a direct fie~d regulator . Since there is a large
overlapping momentum rang<; betl·reen the present instrument and the Ring
Focusing Beta-P~y Spectrometer , and since the latter instrument is pro
vided uith proton resonance units to measure its magnetic field, the
momentum scale of the present instrument can be readily established in
terms of the current in the field coils . The primary calibration of both
instr~~ents rests on the wavelength measurements made with the curved
crystal ganuna- ray spec·0rometer .
The pr~n~ry pmrer for the 180° spectrometer magnetic fiel d
coils is obtained from a motor- generator set operating from 220 v ac
and proYiding up to 4 amperes at 250 v de. The spectrometer field
current also flows through a small solenoid mounted on the base of the
current stabilizer (see Fig. 4) '1-·Thich provides a magnetic field propor
tional to the spectrometer field . A ci rcular coil rotating in this field
forms a small ac generator . This is the sensL~g generator . On the same
rotating shaft is another coil operating in a fixed magnetic field pro
vided b~r an Alnico Jllagnet . This is the reference generator . The output
of the reference generator is divided by a precision potentiometer
mounted on the same rotating shaft . The divided output of the reference
generator and the output of the se~ing generator are connected in series .
The sinusoidal signals from the reference and sensing generators are
adjustable to be exactly 1eo0 out of phase so as to furnish the error
signal vThich is used to stabilize the current produced by the main de
generator . In order to get the error signal out of the rotating system
-10 -
":1-lu'
,------------------ -------- - ----------------------------, I I I I I I I I I I I I ____ _________ __ __ I
CONTROL. OIA.L.
SPEC.TROME1"ER ~ F lELOc:.QILS
I L __
A--tA&u•.IG '-'0\..."TAG.a UEC~AN\CA..L U NIT
r/
i,-1------, I I I I L_ ___ _____ _
lt,HXX:.TtON MOTOR aHP
Fig. 4. Current Regulator showing the mechanical unit and the system block diagram.
-11-
to the external circuits a transformer is used whose primary winding
consists of a circular coil of l-vire coaxial w-ri th and rigidly fastened to
the rotating shaft . The secondary \vinding is also coaxial Hi th the shaft
but is stationary. This trffi1sformer avoids the necessity for slip rings
and brushes •-<hose sliding contacts might introduce i..'1stabili ty in the
error signal .
The ac error signal null indicates equality of the sensing
generator output and the divided output of the reference generator . -The
dividi..'1g potantiometer is a ten- turn Helipot vihich, as before stated,
rotates with the shaft . The setting of this rotating potentiometer is
made through a double differential gear train .
Since the e~or signal is an alternating signal a reversal of
its algebraic sign would be indistinguishable in the external circuits
unless a reference phase signal from the rotating shaft is available .
This phasing voltage is obtained from a vari&ble reluctance generator
operated by the same shaft as the sensing ~•d reference generators . In the external non- rotati ng circuits the ac error signal is amplified and
rectified in a phase s ensitive detector in which the phasing voltage
from the variable reluctance generator serves as a phase reference . This
detector furnishes at its out~ut a correctly polarized de error signal.
Together with a fixed de voltage the de error signal biases control tubes
which provide field current for the primary pm-ver generator .
The system constitutes a servo-mechanism which regulates the
spectrometer field current by tending to maintain equality between the
sensing generator output and the divided outnut of the reference genera
tor. Control of the stabilized current is achieved by operating the
dividing potentiometer. 7he relative accuracy of current measurement
with this system depends on the constancy of the reference generator out
put , the sensi tivity of the sensing ger.erator ffid the linearity of the
dividing potentiometer . Table II gi ves the specifications of the regu
lator components .
Tests have shovm the inherent stability of the system to be
\..Ji thin + 2 parts in 10 ,ooo. The lineari t:r is determined by the precision
potentiometer which is claimed by the manufacturer to be linear within
~ 2.5 parts in 10,000.
-12-
TABLE II SPECIFICATIONS FOR CURRENT REGULATOR COMPONENTS
Earth's Field Compensation C0ils for Sensing Generator
Vertical 1300 turns of #33 formvar wire; 820 ohms; mean s~\are side 8-3/16 inch; .3 gauss
Horizontal 1000 turns of #33 formvar Hire; 463 ohms; mean square side 6 inches; .3 gauss
Reference Generator JL~ature
1400 turns #40 enameled copper; 370 ohms; mea..1 diameter 7/8 inch
Sensing Generator Armature
2800 turns #40 enameled copper; 2300 ohms; mean diameter 2-3/4 inch
Sensing Generator Sole:.:.0id (each of tlvo coils)
216 turns #20 heavy formvar copper; 1.8 ohm; 25 gauss at 2 amps
Rotating Transformer (mild steel core; air gap~ 10% of total reluctance)
Primary
Secondary
11,000 turns; #36 enameled copper; 2200 ohms
16, 500 t Jtl38 1 d 800 hm urns ; , ename e copper; o s
Variable Reluctance Generat or (each of tl-ro cojls connected in series)
11,000 tun1s #38 enaT"leled copper; 3500 ohms
Magnet (shaded) is \·Tater hardened Ketos . By momentarily connecting ungrounded side of phasing connector on control chassis to + 380 V de the Ketos steel is magnetized to proper strength and direction . Renainder o: core is mild steel. Haximum series O'~tput of generator (vrith 0 .5 mfd. across output) is about 8 V ac with minimum clearance bet1·1een wedge armature and core . Normal output set at 3 V ac by increasing clearance.
-13-
C. Compensating Coils for Earth 1 s Magnetic Field
The sensing generator output of the current stabilizer is
affected by the t1·10 components of the earth's magnetic field perpendicular
to the shaft . The component parallel to the shaft has no effect at all .
The horizontal component, perpendicular to the sensing solenoid, causes
a phase shift between the sensing generator and reference generator out
puts . The vertical component causes a change in calibration of the
regulator . To eliminate the stray field components tuo pairs of Helm
holtz coils are mounted around the sensing solenoid. Table II includes
the specifications of these compensating coils.
Adjustment of the current in the Helmholtz coils is achieved
by disconnecting the refe~ence coil and running the sensing generator.
The output i s observed on an oscilloscope and a null is obtained when the
stray field is cancelled out.
Since t he main spectrometer field is not measured directly,
it is also necessary to cancel out the vertical (axial) as well as the
horizontal components of the earth's magnetic field over the region of
electron trajectories .
The horizontal component of the earth's field is cancelled
in this case by the two pairs of square Helmholtz coils seen in Fig. 1 .
Each pair consists of t vro scr1are frames made of aluminum channel. The
corners clip together and each coil form is notched so that the four
coils clip to each other and to the main framework of the spectrometer.
The vertical component of the earth's field is cancelled by
a pair of circular coils wound on the sealing rings of the main coils as
shown in Fig. 3.
An air-driven generator is us ed as the detector to determine
the current settings required to eliminate stray magnetic fields in the
vicinity of the electron trajectories .
Table III gives the specifications of the three pairs of
spectrometer compensating coils .
-14-
TABLE III SPECIFICJ..TIONS OF SPECTROHETER CO?-iPENSATING COilS
Each Coil Round Coil (Vertical) Square Coil (Horizontal)
\vire size #33 (formvar coated) #33 (formvar coated)
Number of turns 1000 1000
Resistance 2100 ohms 1600 oh1ns
Insulation Glass tape Glass tape
Cross section 1/2 in. X 1/2 in. 1/2 in. X 1/2 in.
Coil form Cast brass Aluminum channel
Field strength (pair) 0 to 0. 5 gauss 0 to 0.5 gauss
- 1.5-
D. ~ectrometer Chamber
The vacuum chamber is machined from a solid aluminum forging .
The front is provided Hith t~vo round holes, one for the source and the
other for the Geiger counter . The source and the counter are each
mounted on circular aluminum plates which cover these holes and clamp to
the chamber with thumb screws . The mounting plates are located by bronze
dowel pins as shown in Fig • .5a. The solid angle of the electron trajec
t ory is determined by the \·lidth of the diaphragm shmm in Fig • .5b . To
change the solid angle the diaphragm is slid out and an appropriate one
inserted. A vacuum lock surrounds the counter to protect the thin window
when the chamber is open to the atmosphere. The clapper valves on the
vacuum lock and in the main vacuum line (this valve may be seen in Fig. 1)
are closed during the insertion of the source. A high vacuum port is
provided in the vacuum lock so that a small leak over a long period of
time would not endanger the counter l-Jindow. Fig • .5 also shows the lead
shielding betHeen the source and the counter .
1 . Source
The s ource ~s prepared by first evaporating a layer of the
radioactive material , of the order of atomic thickness, on one side of a
thin mica sheet . A thin layer of aluminum is evaporated over the source
material to remove the positive charge that builds up on the source as
the negative electrons are ejected. I n cases vrhere the absorption by
the aluminum is significant, the process is reversed: the aluminum is
evaporated directly on the mica sheet and then t he radioactive material
i s evaporated on the alUML~~~ surface . For a standard momentum resolu
tion of 0 . 8% a strip is cut from t he prepared mica sheet 0 .1 em x 4 em.
This strip is cemented to an alumim.un support between two engraved lines .
The aluminum support is located on the source holder with two pins ~~d
held by two scrm-1s as shmm in Fig. 6.
·-16-
Fig. 5. Spectrometer chamber (with cove r removed).
--17-
Fig. 6. Radioactive source and holder.
-18-
2 . Geig~ Counter
The Geiger counter (shown in Fig. ?) is machined froM one
piece of aluminum. The width of the vrindow is varied for different reso
lutions by replacing the front plate viith one having the desired aperture
width. The window itself mus t be thin enough to allow transmission of
lm1 energy electrons and yet must support a pressure of approximately
10 em of Hg. The vrindow material used is formvar . A solution of 4% fo~var in ethylene dichloride is prepared. A clean glass plate is im
mersed and witr.draHn and the solution is allowed to run off, leaving a
thin film on the surface of the glass . '\ilhen the formvar film has set it
is peeled up at the edges by the use of a razor blade and floated off in
a beaker of water. The aperture ~late is passed under the floating film,
and the film adheres t o the plate as it is removed from the water .
The 4% formvar solution gives a windmv thickness of the order
of 10 1-Lg/ cm2, Hhich allot-Is trans.11ission down to an electron energy of
2 kev. Usually tlvo layers of formvar film are used to minimize the leakage
of counter gas vJhich may occur 1-1i th s uch a thin film .
The filli~b gas for the coa~ter is a mixture of 2 em Hg of
alcohol vapor and 4 em Hg of argon.
} . Installation of the ~ectrometer Chamber
A flat cover completes t~e ch&llber assembly. All mating sur
faces are sealed vTi th neoprene 110 11 rings except those in contact with the
alcohol- argon mixture . These are sealed Hith teflon gaskets to p revent
contamination of the colli!ter gas with dissolved hydrocarbons from the
rubber "0" rings .
The chamber asser:bly is mounted on a base plate with bronze
screws and located by t >vo bronze dm.;el pins . The base plate is adjustable
in the vertical di::-ection by the use of three adjusting screws and in the
horizontal direct ion by slots in the base plate and the main frame work.
The base plate is made parallel to the plane of the main field coils and
its vertical position set by the use of an inside rr~crometer . The chamber
is clamped to the base plate and is lined up coaxially Hith the main coils
by use of a plumb line suspended from the main frame .
-19-
Fig. 7. G. M. Counter
-20-
E. Vacuum ~ystem and Geiger Counter Filling ~ystem
The complete vacuum and counter filling system is shown
schematically in Fig. 8. A Welsh 30 liter/min. duoseal mechanical
pump provides the fore vaaL~um for the 60 liter/sec. oil diffusion
pump , 1-1hich achieves a vacuum of the order of 5 x lo-6 mm of Hg.
The cold cathode Phillips type ionization gauge has a range of 0.5 to lo-7 mm of Hg and is unaffected by atmospheric pressure . A set
of baffles protects the Phillips gauge from contamination by the oil
vapors from the diffusion pump. At B is a clapper type . 10\-T impedance
valve which is closed when the source holder is removed, leaving the
spectrometer c hamber open to the atmosphere. During this period the
vacuum lock clapper valve .b. is also closed. Valve C is al-vrays open,
mai ntaining a vacuum around the outside of the counter window except
when the windorr is being replaced. These three valves (A, B, and C)
allm1 the spectrometer to be opened and still maintain a vacuum in the
rest of the system, rett~cing the pumping time required to evacuate the
spectrometer chamber again.
Valves C, D, E, and F are the diaphragm type -v1ith a Kel-F
seal (Hoke Hodel 48 2). V a: ve G is the diaphragm type with a neoprene
seal (Crane J.Vlodel 1600) . All lines are copper or glass tubing. Per
manent joints are soldered or fuvar- fused to glass . Removable connec
tions are sealed with neoprene "0 11 rings or Teflon gaskets .
To pump dorm the spectrometer chamber, valve G is closed
and E is opened. This permits the by-passing of the diff1sion pump ,
eliminating the necessity of an additional mechanical pump . After a
feH minutes the by-pass valve, E, is closed, G is opened, and clapper
valves A and B may be opened.
To r emove the source, t i1e cl apper valves A and B are
closed and valves D and Fare openedtobring the spectrometer chamber
to atmospheric pres sure.
To r eplace the Geiger counter '"indm-1, with the vacuum
pumps in operation and valves C, B, and E closed, the following
procedure is follov1ed: Install the ne-w window and clamp the counter
in place . Close valves G and F. Open valves A, D, K, and H. Open
I I I L
G. M. counter
-21-
SPECTROMETER CHAMBER
ballast tank
B
baffle
diffusion pump
G
-, I I I
_J
E
COUNTER FILLING SYSTEM
H
I
monoalcohol meter
._- _.J
Bourdon gauge
D
fore pump
Fig. 8. Schematic diagram of vacuum and G . M. counter filling system.
F
atmos. or
argon
-22-
valve E slowly to pe~~it the interior of the counter and the spec
trometer chamber to be pumped dovm at the same rate. The Bourdon
Gauge gives a good indication of the pu."!lpi.."lg rate . \'lhen the system
has been rcughed dmm to 0.5 mm of Hg, close valve E and open G and
B. This allrn-vs the diffusion pump to continue the evacuation more
quickly.
To fill the ccunter, close valve D and K. Open valve I
to the alcohol until the mercury ~anometer reads 2 em. Close I and
open J slowly to admit the Argon until the manometer reads a total of
6 em.
... 2J-
F. Detecting and Recording ~ystem
With the exception of the Geiger counter and the pre
amplifier, the entire detect ing and recording system is built up of
commercial units . The pmver supplJr of a decade scaler (Atomic Instru
ment Co., Model No. 1010) provides the high voltage t o the counter .
The counter pulses are a-mplif ied in a prea-nplifier with a cathode
follower stage to shape the pulse for the counting- rate meter (Detecto
lab, Model .!liT) . The rate mete:· output voltage is fed to a strip chart
recording potentiometer (Heston, 11odel No. 6701) . The chart is driven
by a synchronous motor as is the control knob of the current regulator
for the spectrometer field . Each complete turn of t h e control knob
sends a signal to the recording potentiometer so that an automatic
record is made of beta- ray momentum versus counting rate.
-24-
III PERFOffi.iAUCE CURVES
Z2
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Fig
. 9
.
CU
RR
EN
T
IN
AM
PE
RE
S
Co
nv
ers
ion
ele
ctr
on
sp
ectr
um
em
itte
d b
y a
Y
b 16
"9 so
urc
e.
Th
e p
eak
s d
ue t
o
gam
ma t
ran
sit
ion
s i
n T
m1
69
are
id
en
tifi
ed
in
th
e f
igu
re.
Th
e m
om
en
tum
re
solu
tio
n i
n t
his
ex
peri
men
t w
as
0.
8o/o.
T
he e
... e
rgy
ran
ge i
s
33
to
83
kev
.
j
1\)
\.11.
I
Fig
. 1
0.
5 w
~4
a::
t93
z 1
--2
z ::>
0 u
2 5
w4
~ 0
::3
t9
z2
1-
z :>I
0 u
3
A
3 B
~
(\J
rt)
(()
4 5
.....
~
(\J
~
<X)
6 E
NE
RG
Y
IN
KE
V
4 5
6 7
EN
ER
GY
IN
K
EV
7
... 0
z
- I (\
J ~
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<X
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8
8
9
9
Tm
'69
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j
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1:1
1"-
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l)
C\J
I':
0 (\J
a _
j ~
0 (\J
10
II
12
Lu
l75
10
II
12
In F
ig.
10
-A i
s s
ho
wn
th
e T
m 1
69
beta
-ray
sp
ectr
wn
, fr
om
2 t
o 1
2.
5 k
ev
fo
llo
win
g
the d
ecay
fro
m Y
b1
69
, as r
eco
rded
on
th
e c
hart
reco
rder
fro
m t
he o
utp
ut
of
the
sem
icir
cu
lar
sp
ectr
om
ete
r.
Th
e u
nla
bell
ed
peak
s are
pri
ncip
all
y L
-Au
ger
lin
es.
T
o i
den
tify
th
e T
m L
-Au
ger
lin
es
in t
his
sp
ectr
wn
, an
in
dep
en
den
t st
ud
y o
f th
e
Lu
L-A
ug
er
sp
ectr
um
em
itte
d b
y H
f17
5 s
ou
rce w
as
un
dert
ak
en
, si
nce i
n t
he L
u1
75
sp
ectr
um
no
co
nv
ers
ion
ele
ctr
on
s o
f lo
w e
nerg
ies
are
pre
sen
t.
Fig
. 1
0-B
rep
resen
ts a
ty
pic
al
ch
art
reco
rdin
g o
f th
e L
ul7
5 L
-Au
ger
sp
ectr
wn
.
I rv
0' i
9 8 7 6 5 C
l) -0 ~ Ol4
c -c :::
J 8 3 2
N1
Nml
NIV
,V 0
l l M
1v,v j
Mm
l Mi'
M1 ~
a~--~~--~--~~--~~~~--~~--~--~~~
.520
.5
00
.4
80
.4
60
.4
40
.4
20
.4
00
F
ield
cu
rren
t in
am
pere
s
Fig
. 1
1.
Co
nv
ers
ion
ele
ctr
on
s o
f 8
. 4
2 k
ev
gam
ma r
ay
in
Tm
16
9 e
xcit
ed
by
Er
16
9 b
eta
d
ecay
. P
ron
ou
nced
Ml,
M
il,
an
d M
ill
peak
s w
ith
6.
1,
6.
33
, an
d 6
. 5
3 k
ev
ele
ctr
on
en
erg
y r
esp
ecti
vely
can
be s
een
, in
ad
dit
ion
to
N a
nd
0
co
nv
ers
ion
p
eak
s.
Th
e s
ou
rce u
sed
in
th
is e
xp
eri
men
t w
as
ob
tain
ed
by
vacu
um
ev
ap
ora
ti
on
on
an
Al
co
ate
d m
ica s
heet,
as d
escri
bed
in
th
e t
ex
t.
Th
e l
ines
ob
tain
ed
are
pra
cti
call
y f
ree o
f re
tard
ati
on
"ta
ils 11
at
low
en
erg
y s
ide.
Th
e s
ou
rce w
idth
w
as
1 m
m.
Th
e c
ou
nti
ng
rate
on
th
e p
eak
of
the M
I li
ne w
as
ab
ou
t 1
00
0 c
ou
nts
p
er
min
ute
. F
rom
th
e p
resen
t M
su
bsh
ell
co
nv
ers
ion
sp
ectr
um
it
can
be c
on
clu
ded
th
at
the 8
. 4
2 k
ev
tra
nsit
ion
in
qu
est
ion
has m
ixed
MI
+ E
2 m
ult
ipo
lari
ty.
I 1
\)
-.J I
w .....
5 4
<I
3 a::
(!
) z .....
z :::>
0 2
(.)
Pt
Lm-M
v M
1v,v
~
Pt
Lm-M
v M
m
Os
L111
-Mv
M1v
,v \
Os
Lm-M
v M
m
Pt
Lm-M
v M
u " --
Pt
and
Os
L-A
ug
er
Pt
Lu-M
v M
1v, v
/
O
5 6
7 8
9 10
II
12
13
Fig
. 1
2.
EN
ER
GY
in
ke
v
L-A
ug
er
ele
ctr
on
sp
ectr
um
em
itte
d f
rom
an
Ir
19
2 so
urc
e.
Sin
ce I
r 1
92
decay
s b
y
ele
ctr
on
cap
ture
to
Osl9
2 a
s w
ell
as b
y b
eta
decay
to
Ptl
92
, A
ug
er
ele
ctr
on
s o
rig
inati
ng
in
Os
an
d P
t ato
ms
are
pre
sen
t; t
he P
t A
ug
ers
are
, h
ow
ev
er,
d
om
ina
tin
g.
Th
e s
ou
rce u
sed
here
was
pre
pare
d b
y v
acu
um
ev
ap
ora
tio
n a
nd
has
lin
ear
dim
en
sio
ns
of
on
ly 0
. 5
mm
tim
es
7 m
m.
Max
imu
m r
eso
luti
on
of
0.
8%
is a
ch
iev
ed
, b
ut
in v
iew
of
the c
om
pli
cate
d s
pectr
um
bett
er
reso
luti
on
wo
uld
be d
esi
rab
le.
Ten
tati
ve i
den
tifi
cati
on
of
the p
eak
s is
giv
en
.
N
())
I
-29-
APPENDIX
Magnetic Field Study
When the main magnetic field coils were assembled on the
spectrometer framework th~ field was mapped using a one inch diameter
flip coil and a ballistic galvanometer . Fig . 13 shows the axial com
ponent of the field plotted along a line in the Z = 0 plane, passing
through the Z axis of Fig. 2. Eacn curve represents a different coil
spacing (L). Curve (a) shows the field obtained with the coils spaced
according to the Helmholtz condition, L = r , where r is the radius of c c each coil (r = 34 em). In curve (b) the coils are moved closer together
c (L = 32 em) . The maxlimun is no longer at r = O, but is at approximately
r = 5 cmo In cu~ve (c) (L = 29 em) the maximum is at r = 12 em~ This
is the optimQ~ spacing for the given coil diameter (63 em) and an elec
tron trajectory radius of 12 em. A spacing of less than 29 em moves the
maximum out beyond r = 12 em as sho1-m in (d) .
If points 11?1'1 in Fig. 13 are connected a curve is obtained
which gives the radius of tha ~~ular region of uniform magnetic field
versus coil spc-.cing. Fig. 14 shows this curve with dimensionless co
ordinates. For a given pair of coils, multiply the coordinates by the
coil radius and read off the proper spacing for any radius electron
trajectory.
This was done for the present case, using the mean coil
radius (34 em) and the mean radius of the electron trajectories (12 em)
which gives a coil spacing of 25.4 em. A plot of the axial component
of the field was made in a plane through the axis of the coils. Fig. 15 shows this as a family of constant flux lines . The rectangle represents
the cross-section of the electron trajecto:i:'i'3s at the Hidest part of the
beam. Point M is the max.imu.'ll shovm in Fig . 13.
The gradient that exists in the region of the electron
trajectories contributes to second order focusing of the electron beam.
If the magnetic field ~ere perfectly homogeneous then, in Fig. 16 the
central trajectory, c, would enter the counter window slightly to the
-30-
Appendix, continued
right of trajectories A and B. With the field distribution as shown
in Fig. 13-c, the field at A and B is less than at C and thus rB and
rA become ~eater than rc' moving the focus of the extreme trajectories
closer to the focus of the central beam c. In the present instrument
the gradient is not sufficient to achieve complete second order focusing.
-31-
M
{a) L= 34 em. r=O
M
{b) L= 32 em.
r = 5 em.
M
{c) L= 29 em.
r = 12 em. M
{d) L= 28 em.
r = 14 em.
Fig. 13. Curves of axial component of magnetic field plotted along a horizontal line, through the axis, midway between the two main coils. Each curve represents a different coil spacing.
-32-
0.6--------------------------------------~
rM~ rc
0.5
0.4
0.3
0.2
0.1
rM= radius of toroidal region of homogeneous field.
'\. rc =radius of field coils.
' '\. L = coil spacing. -'
0 ~------~------~--------------_. ______ __ .75 .80 .85 .90 .95 I. 0
L Ire
Fig. 14. Radius of the toroidal region of maximum magnetic homogeneity for a pair of circular coils versus separation of the two coils. The curve is obtained by passing a line through points marked 11 M 11 in Fig. 13. The dotted portion is not too useful because the height of the uniform region becomes less than the width.
Z a
xis
~1Cl
> ~Cl
>' ~Cl>
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. q
en
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en
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en
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1 l
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-4
2 4
6 8
10
12
14
16
em.
radi
us
Fig
. 1
5.
Plo
t o
f th
e a
xia
l co
mp
on
en
t o
f m
ag
neti
c f
ield
in
a v
ert
ical
pla
ne t
hro
ug
h t
he
cen
tral
ax
is.
Th
e d
ista
nce b
etw
een
th
e i
nd
ucti
on
lin
es
rep
resen
ts a
fl
ux
d
iffe
ren
ce o
f l.
5 p
art
s i
n 1
00
0.
Th
e d
ott
ed
recta
ng
le i
nd
icate
s th
e m
ax
imu
m
wid
th o
f th
e e
lectr
on
beam
.
I w
w i
-34-
B
Fig. 16. Second order focusing.
FA,B Fe counter
lj ;,n:
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. 1
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40
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