For photometry of point-sources the power on the detector is decribed by:
is the flux of the point source in at the selected wavelength; is the fraction of the point spread function which passes through the aperture and can be found in Table 2 and 4 of the IOM3.1. C1 is a wavelength dependent parameter and is tabulated in Tab. 2. The following parameters are represented by the factor C1:
For extended sources the total power depends on the surface brightness of the source and the solid angle of the aperture, thus:
where is the flux density of the extended source in , e is the obscuration factor by the secondary mirror of the ISO telescope, where , and is the solid angle of the aperture or array projected on the sky. The values for can be found in Table 1.
The total noise is described by the following equation:
This includes an additional measurement for background subtraction so that the background and read-out terms are counted twice.
is the photon noise for a point source:
Table 1: Solid angles for PHT-P and PHT-S apertures and for individual pixels of the PHT-C arrays. For PHT-C detectors the individual pixel sizes are given in parentheses.
PHT-P apertures | PHT-S aperture | |||
[ ] | ||||
5'' | 0.00461 | 24 24'' | 0.1354 | |
7.6'' | 0.01066 | |||
10'' | 0.01846 | |||
13.8'' | 0.03515 | |||
18'' | 0.05980 | |||
23'' | 0.09764 | |||
20 32'' | 0.14840 | |||
52'' | 0.49907 | |||
79'' | 1.15189 | |||
99'' | 1.80896 | PHT-C arrays | ||
120'' | 2.65779 | (per pixel) | ||
127 127'' | 3.73997 | C100 (43.5''x43.5'') | 0.44468 | |
180'' | 5.98002 | C200 (89.4''x89.4'') | 1.87820 | |
For extended sources the photon noise is:
The noise induced by the background is described by the same formula, except that becomes the flux density of the background:
is the detector noise and can be represented by a constant for each detector:
Table 2: PHT-P and PHT-C In-flight sensitivity characteristics. The sensitivity parameters C1, C2 and C3 are defined in the equations given in this section.
filter | C1 | C2 | C3 |
[ ] | [ ] | [ ] | |
P1 | |||
3.29 | 1.5 | 1.7 | |
3.6 | 7.1 | 3.8 | |
4.85 | 7.3 | 3.8 | |
7.3 | 9.8 | 4.5 | |
7.7 | 2.0 | 2.0 | |
10 | 2.3 | 2.2 | |
11.3 | 0.79 | 1.3 | |
11.5 | 4.7 | 3.1 | |
12.8 | 1.6 | 1.8 | |
16 | 0.80 | 1.3 | |
P2 | |||
20 | 5.1 | 3.4 | |
25 | 4.6 | 3.2 | |
P3 | |||
60 | 0.60 | 0.70 | |
100 | 0.88 | 0.85 | |
C-100 | |||
50 | 0.51 | 0.12 | |
60 | 0.66 | 0.13 | |
70 | 0.73 | 0.14 | |
90 | 1.53 | 0.20 | |
100 | 0.96 | 0.16 | |
105 | 0.61 | 0.13 | |
C200 | |||
120 | 0.31 | 0.29 | |
135 | 0.72 | 0.44 | |
160 | 1.05 | 0.53 | |
180 | 0.55 | 0.38 | |
200 | 0.23 | 0.25 | |
Now the integration time can be calculated from Eqn. 2. The constants C1, C2, and C3 are tabulated in Table 2. The constants C1 and C2 have been determined from a signal and noise analysis of relatively long staring measurements of calibration stars ( sec). C3 is normally determined from a noise analysis of dark measurements. For consistency with IOM3.1 we include in this term uncertainties the observer will face with faint source measurements, like flat-field accuracy, signal drifts, and also partly sky structure, when subtracting the considerably brighter background. These have been obtained from dedicated faint source measurements. Scaling sensitivity limits from longer measurement times to shorter ones (of less than 128 sec) does not always follow Eqn. 2, see Section 5 for more detail.