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Lifetime measurement of the first excited state in 22Ne
H. Sztark, J.L. Quebert, P. Gil, L. Marquez
To cite this version:
H. Sztark, J.L. Quebert, P. Gil, L. Marquez. Lifetime measurement of the first excited state in 22Ne.
Journal de Physique, 1972, 33 (10), pp.841-845. �10.1051/jphys:019720033010084100�. �jpa-00207314�
LIFETIME MEASUREMENT OF THE FIRST EXCITED STATE IN 22Ne
H.
SZTARK,
J. L.QUEBERT,
P. GIL and L.MARQUEZ
Centre d’Etudes Nucléaires de
Bordeaux-Gradignan, IN2P3,
Le
Haut-Vigneau, 33-Gradignan (Reçu
le 20 mars1972,
révisé le 2juin 1972)
Résumé. 2014 La vie moyenne du
premier
état excité de 22Ne(2+,
1,277MeV)
a été mesurée par la méthode du parcours derecul,
à l’aide de la réaction19F(03B1, p03B3)22Ne
à basseénergie :
les rayonne- ments 03B3 ont été détectés en coïncidence avec les protons émis à 170° du faisceau incident. La vie moyenne trouvée est : 03C4 =(5,9 ± 0,6)
ps.Abstract. 2014 The mean lifetime of the first excited state of 22Ne
(2+,
1,277MeV)
has been mea-sured
by
the recoil distanceDöppler-shift method, using
the reaction19F(03B1,
p03B3)22Ne at low energy.The 03B3-rays were recorded in coincidence with the protons emitted at 170° to the incident beam.
The mean lifetime was determined to be : 03C4 =
(5.9 ±
0.6) ps.Classification : Physics Abstracts 12.00, 12.13, 12.20
1. Introduction. -
Among
the nuclear informations that can be deduced fromexperiment,
the lifetimesof the excited states are
directly
connected with nuclear modelsby
means of the reduced transitionprobabilities.
In theregion
between10-10
and10-12
s, the «recoil-shift méthode[1], [2], [3]
isthe
only
one which hasproved
to besufhciently
accurate.
Indeed, by
this method the average recoilvelocity
can beaccurately
knownby measuring
theenergy difference between the y-rays emitted
by
recoil-ing
andstopped
nuclei.We
adjusted
thistechnique
to very lowenergies
with 2.9 and 4 MeV
a-particles
asprojectiles,
and weapplied
it to the 1.27 MeV state of22Ne :
the meanlifetime enables us to calculate the
B(E2, 0+ - 2+)
of the 1.27 MeV
level,
that we havecompared
withprevious
results onquadrupole
moments,using
therotational model.
II.
Expérimental
method. - Theexperiments
havebeen
performed
at the 4 MeV Van de Graaff from the CEN deBordeaux-Gradignan.
Because of thelow incident energy, we had to choose an
exoergic
reaction to
get
a recoilspeed
sufhcient for the studiednucleus. We used the reaction
19F(a, p) 22 Ne,
whoseQ-value
is 1.698MeV,
at two incidentenergies :
2.9 and 4
MeV,
with a beam of about 50 nAintensity.
The thin
targets
ofF2Ba (30 Jlg/cm2)
wereevaporated
onto a copper foil 1 gm thick : this was then stretched
to
get
a surface as flat aspossible.
The
recoiling
nuclei werestopped by
a brassplun-
ger, movable with
regard
to thetarget,
the surface of which wasthoroughly parallel
to the stretchedtarget :
the distance d betweentarget
andplunger
is
determined by measuring
thecapacitance
betweenthese two
surfaces,
and was known with an accuracy of ± 1.5 gm.The y-rays emitted
by
therecoiling
nuclei wererecorded
by
a 60cm’ Ge(Li)
coaxial detector at 0°to the beam : this detector has a resolution of 2.5 keV for the 1.27 MeV
22Na
line.To
get
agood separation
of the twoy-lines
and agood
definition for the recoilvelocity,
the y-rays wererecorded in coincidence with the backscattered
protons
associated with therecoiling
nuclei. Theseprotons
are detected with a surface barrier
ring-counter,
at180° to the incident beam : to
stop
thea-particles
diffused
elastically
at 1800by
the brassplunger,
weput
a 20 gm aluminium foil in front of thering-
counter, the thickness of which was calculated to
stop
the diffused beam and let gothrough
the back-scattered
protons.
The size of the detector defines the directions of the recordedparticles,
and thenthose of the
recoiling
nuclei taken into account :so, the recoil
velocity
is very well established. More-over the coincidence
circuit,
of the multidimensionalkind,
allows us to choose a well defined energy group ofprotons,
andthen,
the y-rayscoming
from thedecay
of a well defined level(the
first of22 Ne
in ourcase) :
so, we can avoidpossible feeding
of the studiedlevel
by
adecay
ofhigher
states.On
figure 1,
one can see the difference between directspectra
for distances d = 6 and 30 gm, and the samespectra
in coincidence withprotons :
we can see theadvantage
of this last method in the definition of the twoy-lines.
From the energy difference AE between the two lines of the coincidencespectra,
we can determineaccuratly
therecoiling
nucleivelocity
v,after correction for the effective solid
angle
at the.Ge(Li)
detector[3].
Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:019720033010084100
842
FIG. 1. - Comparison between direct and coincidence y spectra.
Coincidences are obtained with protons emitted at 170° to the incident beam, at 2.9 MeV incident energy.
In our
experiment,
the direction of therecoiling
nucleus is very well known and no other corrections
are needed. On the
contrary,
if we want to evaluate thisvelocity
from the directspectra
we have to consi- der othercorrections,
as described in reference[1].
We obtained the effective
values, for fi
=v/c :
III. Results and
interprétation.
-1. EXPERIMENTALDATA. -
Figure
2 shows some of thespectra
obtain- ed in coincidence withprotons,
as a function of thestopping distance,
for 4 MeV incident energy. The variations in the relative intensities of the shifted and unshiftedpeaks
can beclearly
seen : allspectra
were normalised tokeep
a same total surface.The same
experiment
was made with a 2.9 MeVincident energy.
For each
distance d,
we calculated the surfaces uand s of the two
y-lines
aftersubtracting
the back-ground,
evaluated on the most distantspectrum (d
= 79.4 pm at 4MeV).
In this kind of measurement, it is necessary to make
a number of corrections as described in reference
[3].
Many
of these corrections arenegligible
in our case ;for
instance,
all corrections due to the variations of solidangles
are verysmall,
because of the very short distances involved. In the same way, the variation in the countereinciency
for the shiftedpeak
leadsto an increase of
0.7 %
in the shiftedpeak intensity.
The most
important
correction is due to the varia- tion of theangular
distribution of the y-rays emittedFIG. 2. - y spectra in coincidence with protons emitted at 170° to the incident beam, for distances d between 9.4 and 79.4 pm. These spectra come from a 4 MeV incident energy.
All the spectra were normalised on the spectrum corresponding
to the higher statistic (d = 23.2 pm) to keep the same total surface (Iu + Is).
by
therecoiling
nuclei. We measured theangular
distribution of the y-rays emitted
by
thestopped nuclei, by using
a thickF2Ba target to stop
the recoil-ing
nuclei.Figure
3 shows theexperimental
resultsfitted with an
expression
of the form :where
Q2
andQ4
are the finitegeometry
correction factors.The
angular
distribution of y-rays emittedby
therecoiling
nuclei is modified and can bewritten,
at 0° :with
This leads to a decrease in the shifted
peak
inten-sity
of 1.5%.
FIG. 3. - Angular distribution of y-rays in coincidence with protons emitted at 170° to the incident beam.
e experimental points normalised by the particle spectrum.
- theoretical curve : W(O) = 1 + a2 P2 (cos 0) + a4 P4(cos 0).
2)
INTERPRETATION. - We assume that the2’
level can
only
be fedby
direct excitation. This is thecase for the reaction studied because the
feeding by higher
states isrejected by
the coincidence method.The
decay
law is :We then have :
where T is the time of
flight corresponding
to thedistance d : T =
d/v.
If we assume no
dependance
in time for theangular
distribution of the y-rays, we have :
which
gives :
In
fact,
a nucleusrecoiling
in vacuum issubject
to the field of its electrons which modifies the
angular
distribution of the emitted y-rays. To take this effect into
account,
we used theexpressions given by
BenZvi et al.
[4],
and the values measuredby
Nakaïet al.
[5]
for theintegral
attenuation coefficientsG2
and
G4 :
The intensities
I.
and7g
can then bewritten,
at 0° :These
expressions
lead to a value of F as a functionof the distance d. A
least-square
fit programgives
thebest value of the mean
life r,
from the corrected valuesF(d)
as a function of the distance.Figure
4 showsthe
experimental
datapoints
forF(d)
versus thestop- ping distance,
for the two studiedenergies :
thestraight
line is the best fit curve.FIG. 4. - Plot of Log
[ (I. iu + is)-l
versus the separation dis- L(iu u -E- 7s)tance between target and plunger. The lower curve displays experimental results at 4 MeV, and the upper one the results at 2.9 MeV. The distance origin is arbitrary, because it is an
adjustable parameter.
|
.2022 experimental points.
- best fit curve.
3. EVALUATION OF THE ERROR IN THE MEAN LIFE i. - The mean life is
dependant
on three expe- rimentalparameters fi
=v/c,
F and d.The error
on f3
iseasily
calculated from the esti- mate of the center ofgravity
of the two rays. For thetwo other sources of error, we simulated a series of
experiments by replacing
in theexpression
of Fagainst d,
theexperimental
results F and dby pseudo-
random
weighted
values. The series of best fits soobtained enable us to extract errors
coming
from theexperimental
values of F and d.844
Results. - After corrections as mentioned above and error calculations
including AT(d, F, B),
wefinally
obtained :
which
gives
the average :IV. Discussion. - After correction due to the internal conversion coefficient as calculated
by
Rose
[6],
the mean lifetimegives
the reduced transitionprobability :
FIG. 5. - Comparison between our results and previous
results. In the lower figure, we show B(E 2) values, in e2 b2 units, for the 0+ -> 2+ transition. In the upper figure are the intrinsic
quadrupole
values in barn. References are as follow : a) Reference [1].b) Reference [7].
c) Reference [13].
d) Our measurement.
e) We calculated Qo with the expressions (3) and (4) using Morand’s [12] results.
f ) Same calculations using Raynal’s [11] results.
g) Reference [8].
h) Our result, using the rotational model and the adopted sign
of Qo.
Figure
5 shows thecomparison
between the value ofB(E 2)
foundby
our measurement with the results foundby
Jones et al.[1] ]
and Eswaran et al.[7].
By using
the rotationalmodel, the
transition pro-bability
isdirectly
connected with the intrinsicquadru- pole Qo
of the rotational band :the static
quadrupole
moment of the studied levelbeing :
The static
quadrupole
momentQ(2+)
was measuredby
Nakaï et al.[5], [8]
and Schwalm et al.[9] using
the reorientation effect
[10].
We havecompared
theseresults with the value deduced from eq.
(1)
and(2).
On
figure 5,
we show thecomparison
between the result of Nakaï et al.[8]
and our result.The intrinsic
quadrupole
moment can also be deduc- ed from the deformation parameters32
and{34.
Using
an axialsymetry
deformation as :the
ground
statequadrupole
moment can be writtenas it follows :
with :
We used the
parameters P2
andB4
obtainedby Raynal et
al.[11] and by
Morand[12]
to calculateQo.
On
figure 5,
are shown our results for radii ro = 1.2 and 1.4 fm.Nakaï’s result is near the value
corresponding
toro = 1.4
fm,
and our result seems close to the valuecorresponding
to ro = 1.2 fm.In
conclusion,
ourexperimental
results seems tobe a
tangible
link intesting
a model between direct measurement onquadrupole
moments and on meanlifetimes. In
spite
of their smalldifference,
the results in both methods withregard
to theirprecision
agree wellenough
in the framework of the rotational model.References
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(K.
W.), SCHWARZSCHILD(A. Z.),
WARBURTON(E.
K.) and FossAN(D. B.), Phys.
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DIAMOND(R. M.),
STEPHENS(F. S.),
KELLY(W. H.)
and WARD
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QUÉBERT
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BEN ZVI(I.),
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DE BOER(J.)
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