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The slope, intercept, and RMS deviation of a linear fit of the energy scale
of the ACIS flight devices are listed in Table 4.5.
Pulse height as a function of energy is fit to the relation
.
Table 4.5: Energy Scale for ACIS Flight Devices
| CCD |
Quadrant A |
Quadrant B |
Quadrant C |
Quadrant D |
| |
Slope |
Intercept |
RMS |
Slope |
Intercept |
RMS |
Slope |
Intercept |
RMS |
Slope |
Intercept |
RMS |
| |
ADU/eV |
ADU |
eV |
ADU/eV |
ADU |
eV |
ADU/ev |
ADU |
eV |
ADU/eV |
ADU |
eV |
| i0 |
0.2636 |
0.81 |
3.75 |
0.2573 |
0.65 |
4.03 |
0.2662 |
0.77 |
3.52 |
0.2582 |
0.60 |
4.06 |
| i1 |
0.2622 |
0.38 |
3.50 |
0.2559 |
-0.09 |
3.97 |
0.2596 |
0.36 |
4.34 |
0.2616 |
0.07 |
3.80 |
| i2 |
0.2731 |
-0.98 |
3.10 |
0.2839 |
-1.07 |
3.35 |
0.2825 |
0.07 |
3.59 |
0.2745 |
0.43 |
3.67 |
| i3 |
0.2582 |
1.19 |
4.68 |
0.2588 |
1.25 |
4.65 |
0.2542 |
1.25 |
4.51 |
0.2592 |
1.09 |
4.55 |
| s0 |
0.2725 |
-0.12 |
4.69 |
0.2677 |
-0.54 |
3.35 |
0.2574 |
0.13 |
4.02 |
0.2565 |
-0.34 |
3.40 |
| s1 |
0.2359 |
-22.00 |
14.80 |
0.2182 |
-27.07 |
22.37 |
0.2234 |
-24.86 |
20.23 |
0.2297 |
-25.33 |
18.84 |
| s2 |
0.2602 |
0.03 |
3.75 |
0.2715 |
0.15 |
5.27 |
0.2640 |
-0.51 |
4.25 |
0.2692 |
-0.54 |
6.33 |
| s3 |
0.2262 |
-17.33 |
11.16 |
0.2158 |
-19.88 |
13.99 |
0.2186 |
-19.65 |
13.18 |
0.2273 |
-22.80 |
13.66 |
| s4 |
0.2328 |
-1.09 |
3.80 |
0.2272 |
-0.58 |
6.16 |
0.2301 |
-0.72 |
5.76 |
0.2391 |
-0.96 |
4.55 |
| s5 |
0.2534 |
-0.16 |
3.09 |
0.2576 |
-0.13 |
3.18 |
0.2601 |
0.18 |
2.70 |
0.2114 |
0.46 |
4.32 |
|
The residual errors from the linear energy scale fit for the front illuminated
devices are shown in Figure 4.5.
The residual errors from the linear energy scale fit for the back illuminated
devices are shown in Figure 4.6.
Note that Figure 4.5 and Figure
4.6 are on different vertical
scales. Random errors for the line center locations are much less than
1 eV.
Figure 4.5: Linear Energy Scale Residuals for the Front
Illuminated Devices
 |
Figure 4.6: Linear Energy Scale Residuals for the Back
Illuminated Devices
 |
The FWHM for the ACIS flight devices is shown in Figure 4.7.
In Figure 4.7 the points for
the front illuminated devices are the average of the four quadrants, while
the points for the back illuminated devices show each quadrant separately.
The values for the front illuminated devices are listed in Table 4.6.
The values for the back illuminated devices are listed in Table 4.7.
The "NA" indicates that a data point is not available. The 277 eV measurement
was made only for the S-array. Many of the DCM energies were taken with
only i3, s1 and s3 on. One of the DCM sets was taken with only the I-array.
Figure 4.7: Average FWHM versus Energy
 |
Table 4.6: Average FWHM (eV) for Front Illuminated Devices
| Energy |
277 |
525 |
1380 |
1487 |
1740 |
1770 |
2035 |
4500 |
4509 |
6399 |
8040 |
| Source |
C-K |
O-K |
DCM |
Al-K |
Si-K |
DCM |
DCM |
DCM |
Ti-K |
Fe-K |
Cu-K |
| i0 |
NA |
50.8 |
NA |
73.7 |
83.7 |
NA |
81.8 |
NA |
120.4 |
145.9 |
169.5 |
| i1 |
NA |
50.9 |
NA |
73.3 |
83.1 |
NA |
80.7 |
NA |
119.9 |
145.1 |
169.7 |
| i2 |
NA |
53.7 |
NA |
77.8 |
89.4 |
NA |
85.6 |
NA |
128.7 |
155.2 |
179.1 |
| i3 |
NA |
49.6 |
67.0 |
71.8 |
81.8 |
77.4 |
79.7 |
114.5 |
118.6 |
144.0 |
168.2 |
| s0 |
45.8 |
54.9 |
NA |
77.3 |
86.7 |
NA |
NA |
NA |
123.5 |
149.8 |
175.7 |
| s2 |
39.6 |
52.0 |
NA |
74.6 |
84.6 |
NA |
82.7 |
NA |
122.6 |
149.0 |
172.2 |
| s4 |
37.3 |
49.8 |
NA |
69.5 |
78.9 |
NA |
NA |
NA |
111.3 |
134.9 |
159.9 |
| s5 |
38.8 |
48.4 |
NA |
69.2 |
79.3 |
NA |
NA |
NA |
113.3 |
137.3 |
161.4 |
|
Table 4.7: FWHM (eV) for Back Illuminated Devices
| |
Energy |
277 |
525 |
1380 |
1487 |
1740 |
2035 |
4500 |
4509 |
6399 |
8040 |
| |
Source |
C-K |
O-K |
DCM |
Al-K |
DCM |
DCM |
DCM |
Ti-K |
Fe-K |
Cu-K |
| s1 |
A |
92.8 |
139.6 |
143.8 |
150.3 |
154.0 |
NA |
205.9 |
209.0 |
232.8 |
242.1 |
| |
B |
82.6 |
128.6 |
135.9 |
140.5 |
147.8 |
NA |
205.3 |
208.6 |
225.3 |
234.5 |
| |
C |
84.9 |
130.1 |
135.5 |
138.2 |
146.4 |
NA |
210.5 |
207.5 |
229.5 |
234.0 |
| |
D |
99.5 |
152.9 |
159.0 |
162.3 |
170.1 |
NA |
233.5 |
235.0 |
264.6 |
275.8 |
| s3 |
A |
73.7 |
104.5 |
96.5 |
105.3 |
103.9 |
115.0 |
141.0 |
147.4 |
167.0 |
180.9 |
| |
B |
72.1 |
101.3 |
95.8 |
102.6 |
102.2 |
110.4 |
145.1 |
150.8 |
170.8 |
185.5 |
| |
C |
70.0 |
102.1 |
94.9 |
102.5 |
102.1 |
112.9 |
140.0 |
143.6 |
161.3 |
176.5 |
| |
D |
89.0 |
131.2 |
124.5 |
135.1 |
134.5 |
149.0 |
193.5 |
199.4 |
227.7 |
241.3 |
|
The spectral resolution as a function of energy for the front illuminated
devices is shown as a solid line in Figure 4.7
and is described by
 |
(4.4) |
Note that here we treat FWHM0 as an empirical parameter.
In the simplest model for spectral resolution (see section 4.1)
one expects
 |
(4.5) |
The expected value of
in silicon detectors at -120
C is
.
FWHM0
and
for each quadrant of each front illuminated device is shown in Table 4.8.
Table 4.8: Average Front Illuminated Devices FWHM0
and
| Chip |
FWHM0 |
 |
| i0 |
26.56 |
0.516 |
| i1 |
26.49 |
0.517 |
| i2 |
26.02 |
0.513 |
| i3 |
23.77 |
0.514 |
| s0 |
32.09 |
0.519 |
| s2 |
25.88 |
0.509 |
| s4 |
29.73 |
0.552 |
| s5 |
27.56 |
0.518 |
|



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Energy Scale Linearity
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Scale and Spectral
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Please address comments and questions to Dr. John Nousek ( nousek@astro.psu.edu
)