INSTRUMENTATION: WATER AND WASTEWATER ANALYSIS 553
contact the succeeding dynodes accelerated by ever higher
voltages. A cascade of a large number of electrons is collected
by the anode of the ninth dynode. The final photocurrent can
be amplified, electronically, before readout. The gain, G, can
be calculated as follows:
G ( fs )^ n (8)
where fs, the secondary emission factor for each stage,
depends on the dynode emissive coating and n is the
number of dynode stages. Using values for fs of 3 to 10 for
older dynode emissive coatings and 50 for newer coatings
and n equal to 9 results in gains of about 10^4 , 10^9 and 10^15 ,
respectively. The response times can vary from 0.5 to 2
nsec (nanosec, 10^ ^9 sec). The dark current can be decreased
considerably by cooling the photomultiplier detector. Since
the dark current is a fairly constant value it may be sub-
tracted or automatically nulled using a potentiometer. The
Cathode
Phototube
Anode
hn
R^
=^10
6 Ω
E = 1V
1 = 10 –6A
FIGURE 6 Simple phototube circuit.
(Reprinted from Ref. (176), p. 441
by permission of Prentice Hall, Inc.,
Englewood Cliffs, New Jersey.)
Incident radiation
Grill
Shield
Tube envelope
0 = Opaque photocathode
1–9 = Dynode = electron multiplier
10 = Anode
1
1
0
2
2
4
4
3
3
5
5
6
6
7
7
8
8
9
9
10
10
11
Focus ring
Semitransparent
photocathode
Internal conductive
coating
Incident
radiation
Faceplate
Focusing electrode
1–10 = Dynodes = Electron multiplier
11 = Anode (b)
(a)
FIGURE 7 Photomultiplier Design. (a) The Circular-Cage Multiplier Structure in a
Side-on Tube and (b) The Linear-Multiplier Structure in a Head-on Tube. (Courtesy of the
General Electric Company.)
C009_005_r03.indd 553C009_005_r03.indd 553 11/23/2005 11:12:21 AM11/23/2005 11:12:21