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TAB
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662
Optoelectronic Devices
0.5
EFFECTIVE QUANTUM EFFICIENCY
0.4
sin
0.3
-
X
0.0
0.4
0.6
: 0.8
1
1.2
1.4
1.6
WAVELENGTH (MICRONS)
. 73
Fig. 24 Effective quantum efficiency (hole-electron pairs/photon) versus wavelength for Ge
and Si photodetectors.
(After Melchior and Lynch, Ref. 39.)
R
0
Ipp[ w]
C
(a)
1
-2
-0
-2 A
R
C
1
Fig. 25
(a) Equivalent circuit and
(b) noise equivalent circuit of a photodiode, where R is the series resistance and C is the
junction capacitance.
(After DiDomenico and Svelto, Ref. 35.)
CPYRGHT
4 Photodetectors
available power for the photo
118
It is interesting to compare E
For a typical photodiode with
a photoconductor with the sar
available power from the phot
from the photoconductor.
The signal-to-noise perform
equivalent noise circuit shown
noise source due to the series
source. The signal-to-noise ra!
Comparing Eq. (44) with Eq.
at high-level detection where
SNR is comparable; at low-lev
however, the SNR of the pho
B. The p-i-n Photodiode
depletion-layer photodetector.
(the intrinsic layer) can be tai
frequency response. A typical
Fig. 26(a). Absorption of ligh
pairs. Pairs produced in the de
will eventually be separated by
external circuit as carriers drif
Under steady-state condition
biased depletion layer is given
where Jar is the drift current
region and Jairr is the diffusior
side the depletion layer in the t
reverse-biased junction. We :
assumptions that the thermal g
surface n layer is much thinn
electron generation rate is give
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...
:
0.2
ơ
4
He-Ne
RUBY
He-Ne
GaAs
YA G
He-Ne
ARGON
1
I
1
*
VISIBLE SPECTRUM
1
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DETECTORS AND DETECTOR SYSTEMS
CPYRGHT
SILICON CHARGED-PARTICLE DETECTORS
characteristics. The detector changes include in-
creased noise and changes in voltage drop across the
load resistor, which require adjustments to the applied
bias voltage, which in turn change the electric-field
strength. Thus carrier trapping and increased detector
noise are degrading to energy resolution.
.
Resolution degradation appears as a broadening of the
response for a monoenergetic source. With increasing
doses of neutrons, charged particles, or fission frag-
ments, the low-energy side of the response peak may
begin to show a definite secondary peak. Continued
irradiation results in further broadening, until, in ex-
treme cases, the multiple peaks may merge com-
pletely. Electron bombardment tends to increase leak-
age current, resulting in excess detector noise, which
broadens response peaks. Some of these damage ef-
fects may undergo a degree of annealing, but there is
always a significant residual deterioration after a suffi-
cient dose has been accumulated.
Partially depleted detectors are more susceptible than
are fully depleted devices to deterioration from radia-
tion damage. Radiation damage for different types of
detectors are compared in Table 2, which gives the
dose for various particles to significantly deteriorate
the detectors.
OPERATING TEMPERATURE
As a rule of thumb, increasing the operating tempera-
ture of a charged-particle detector causes the leakage
current to increase by a factor of 3 for each 10℃ rise,
resulting in a noise-width increase of approximately 1.7
keV per 10°Crise. The upper temperature limit is deter-
mined by the maximum acceptable noise or by the
ultimate breakdown of the detector (usually between
45 and 55°℃). The effects of high-temperature break-
down are permanent and are not covered by the war-
ranty terms. An additional effect is the shift in detector
bias caused by the higher leakage current. This leak-
age current increases the voltage drop across the se-
ries bias resistor, thus lowering the bias voltage across
the detector. When high-temperature operation is
necessary, a constant sensitive depth is maintained
over the entire operating temperature range only if a
totally depleted detector is used with sufficient
overbias to compensate for the drop across the series
bias resistor, which should be as small as possible
(usually 1 to 3 MS2 is adequate).
Decreasing the operating temperature of the detector
reduces junction noise and leakage current. However,
the capacitance of the device is a constant limiting
parameter of the system noise. Another limitation to
successful operation at low temperatures is the expan-
sion coefficient of the detector's component parts. The
expansion coefficient is similar for silicon and for lavite,
the ring in which the silicon wafer is mounted, but is
quite different for the bonding epoxy. Therefore at very
low temperatures the epoxy may crack, causing exces-
sive noise or loss of contact. The probability of low-
temperature damage increases with detector size. For
cooled operation, detectors fabricated with cryogenic
epoxy may be special ordered from ORTEC.
Another effect of decreasing the operating tempera-
ture of a silicon detector is an increase of the average
energy necessary to create an electron-hole pair, E.
Due to a widening of the bandgap of silicon in the
temperature range from 300 K to 80 K, E increases
from 3.62 eV to 3.72 eV. A result of this increase is an
apparent shift in energy of a measured spectroscopic
line. For instance, Fig. 8 shows the apparent peak shift
of the 5.477-MeV 241Am alpha particle peak in the 4.2-
K to 320-K temperature range measured with silicon
charged-particle detectors.
SHOCK AND VIBRATION
Many ORTEC surface-barrier detectors have been
subjected to the shock and vibration tests required for
Table 2. Comparison of Radiation Damage in Silicon and Germanium Particle Detectors
Radiation Damage (particles/cm2)
Type of Detector
Electrons
Fast Neutrons
Protons
Alpha
Particles
Fission
Fragments
Surface barrier
1013
1012
1010
10º
108
Diffusion junction
1013
1012
1010
109
108
Si(Li)
1012
1011
108-10º
Ge(Li)
108-109
#1
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Appr wed FerREY
3
Chap. 39
a
K-S
d
S
E
Fig. 39,-17
ing "arged. (a) Show that the
lif_al volume. (b) Show that
ated by integrating the Poynting
e equal to the rate at which the
energy density for all points within
he Poynting vector point of view,
zh the wires but through the space
we must first find B, which is the
=ing the charging process; see Fig.
CPYRGHT
Nature and Propagation of Light
CHAPTER 40
40-1 Light and the Electromagnetic Spectrum
Light was shown by Maxwell to be a component of the electromagnetic
spectrum of Fig. 40-1. All these waves are electromagnetic in nature and
have the same speed c in free space. They differ in wavelength (and thus
in frequency) only, which means that the sources that give rise to them and
the instruments used to make measurements with them are rather different .*
The electromagnetic spectrum has no definite upper or lower limit. The
labeled regions in Fig. 40-1 represent frequency intervals within which a
common body of experimental technique, such as common sources and com-
mon detectors, exists. All such regions overlap. For example, we can pro-
duce radiation of wavelength 10-3 meter either by microwave techniques
(microwave oscillators) or by infrared techniques (incandescent sources).
Frequency, cycles/sec
10ª
104
10°
10ª
1010
102
1014
1016
10 18
1020
1022
Visible
Power
-...
Infrared
Ultraviolet
Gamma rays
Radio
10°
104
10$
1
10-3
10-4
10-8
10-8
10-10
10-12
10-44
Wavelength, meters
Fig. 40-1 The electromagnetic spectrum. Note that the wavelength and frequency
scales are logarithmic.
* For a report of electromagnetic waves with wavelengths as long as 1.9 X 107 miles
the student should consult an article by James Heirtzler in the Scientific American for
March 1962.
993
x-rays
Microwaves
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Chap. 4(
994
NATURE AND PROPAGATION OF LIGHT
wolet
yellow orange
md
100
8
80
Relative sensitivity
60
-40
20
0
400
450
500
550
600
650
700
Wavelength, mu
· Fig. 40-2 The relative eye sensitivity of an assumed standard observer at different wave-
lengths for normal levels of illumination. The shaded areas represent the (continuously
graded) color sensations for normal vision.
"Light" is defined here as radiation that can affect the eye. Figure 40-2,
which shows the relative eye sensitivity of an assumed standard observer to
radiations of various wavelengths, shows that the center of the visible region
is about 5.55 X 10-7 meter. Light of this wavelength produces the sensa-
tion of yellow-green .*
In optics we often use the micron (abbr. u) the millimicron (abbr. mu),
and the Angstrom (abbr. A) as units of wavelength. They are defined from
1 = = 10-6 meter
1 mu = 10-9 meter
1 A = 10-10 meter.
Thus the center of the visible region can be expressed as 0.555 u, 555 mu, or
5550 A.
The limits of the visible spectrum are not well defined because the eye
sensitivity curve approaches the axis asymptotically at both long and short
wavelengths. If the limits are taken, arbitrarily, as the wavelengths at
which the eye sensitivity has dropped to 1% of its maximum value, these
limits are about 4300 A and 6900 A, less than a factor of two in wavelength.
The eye can detect radiation beyond these limits if it is intense enough. In
many experiments in physics one can use photographic plates or light-sensi-
tive electronic detectors in place of the human eye.
* See "Experiments in Color Vision" by Edwin H. Land, Scientific American, May
1959, and especially "Color and Perception: the Work of Edwin Land in the Light of
Current Concepts" by M. H. Wilson and R. W. Brocklebank, Contemporary Physics,
December 1961, for a fascinating discussion of the problems of perception and the distinc-
tion between color as a characteristic of light and color as a perceived property of objects.

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