Subsystem PHT-P was a multi-filter, multi-aperture photopolarimeter with
single element detectors and wide beam (up to 3arcmin) capability for
faint extended sources. The covered wavelength range was
3-130
m.
The PHT-P detectors were each located inside an integrating cavity
and had a dimension of 1
1
1mm
.
This subsystem was designed for sensitive, high precision photometry
and polarimetry, using three different detector types
(in parenthesis the detector material is given):
No. | Filter | ![]() |
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min. aper. | scientific objective |
# | [![]() |
[![]() |
[![]() |
[![]() |
[![]() |
|||
P1 | ||||||||
1 | P3.29 | 3.3 | 3.30 | 0.22 | 0.10 | 2.8 | 5 | PAH |
2 | P3.6 | 3.6 | 3.59 | 0.99 | 0.14 | 3.0 | 5 | cosmological gap, |
common to ISOCAM | ||||||||
3 | P4.85 | 4.8 | 4.86 | 1.55 | 0.16 | 4.1 | 5 | continuum to #1, #4 and #5 |
4 | P7.3 | 7.3 | 7.41 | 3.38 | 0.28 | 6.2 | 7.6 | 6.2, 7.7, 8.6![]() |
5 | P7.7 | 7.7 | 7.66 | 0.82 | 0.25 | 6.4 | 7.6 | PAH |
6 | P10 | 10.0 | 10.00 | 1.80 | 0.35 | 8.4 | 10 | silicate feature |
7 | P11.3 | 11.3 | 11.36 | 0.81 | 0.29 | 9.5 | 10 | PAH |
8 | P11.5 | 12.0 | 11.88 | 6.53 | 0.48 | 10.0 | 10 | IRAS 12![]() |
common to ISOCAM | ||||||||
9 | P12.8 | 12.8 | 12.82 | 2.31 | 0.52 | 10.8 | 10 | continuum to #7 |
10 | P16 | 15.0 | 15.16 | 2.84 | 0.35 | 12.7 | 13.8 | general purpose |
P2 | ||||||||
11 | P20 | 20.0 | 21.03 | 9.03 | 0.32 | 17.7 | 18 | close to standard Q band |
12 | P25 | 25.0 | 23.80 | 9.12 | 0.38 | 20.0 | 23 | IRAS 25![]() |
P3 | ||||||||
13 | P60 | 60.0 | 60.85 | 25.89 | 0.11 | 50.3 | 52 | IRAS 60![]() |
14 | P100 | 100.0 | 102.44 | 39.55 | 0.31 | 83.9 | 79 | IRAS 100![]() |
Any combination of apertures and filters was allowed.
Polarisers were only used with the P2 25m filter and the
aperture.
At long wavelengths the Airy disc is significantly larger than the
smallest aperture available. The diameter of the Airy disc
is
=0.84
[
m].
The selection of apertures much smaller than
was
not recommended (see Table 2.2).
Section 2.9 gives more details about the calculation
of
,
and
.
Polarisers: 0, 120 and 240 degrees
Apertures: 5.0, 7.6, 10, 13.8, 18, 2032, 23, 52, 79, 99, 120, 127
127 and 180 arcsec. All apertures are circular except if noted.
The precision of the ISO pointing had implications on the achieved
photometric accuracy. When observing with the smallest PHT-P apertures
(5.0 and 7.6
), the source might have been observed
strongly off-centre,
see `ISO Handbook, Vol. I: ISO - Mission & Satellite Overview',
[20] for details about the ISO
pointing accuracy.
PHT C100 was a array of Ge:Ga with
0.7
0.7
1mm
elements.
Increased photon absorption was achieved by total reflection of
a 30
wedged pixel surface and an integrating cavity. The telescope
beam was fed into these cavities by
mm
anti-reflection
coated germanium fabry lenses mounted with 100
m spacing which
resulted in an optical fill factor of 93%. The effective size of the
pixels on the sky was 43.5
43.5arcsec
, the distance
between the pixel centers (`pitch') was 46.0arcsec.
Throughout this manual the individual C100 pixels/detectors are labelled as in Table 2.4 where the +Z direction is upwards, and +Y is to the left. This corresponds to the projection of the array on the sky. The numbers (1...9) in Table 2.4 refer to the labelling and array counting in ERD, SPD and AAR products.
PHT C200
consisted of 4 pixels arranged in a matrix.
The telescope beam was concentrated on the four detector pixels
by anti-reflection coated
germanium Fabry lenses of 3.9
3.9mm
. The detector crystals
were mounted in an integrating cavity and had prismatic shape to increase
photon absorption. The sizes of the detector pixels themselves were
approximately 1mm
. The effective size of the pixels on the sky was
89.4
89.4arcsec
, the distance between the pixel centers
was 92.0arcsec.
The pixels were stressed by individual screws (Wolf, Grözinger & Lemke
1995, [58]);
the stress was maximized in order to give a cut-off wavelength of
240m. The labelling of the individual C200 pixels is given in
Tables 2.5 and 2.6 for the ERD and
SPD/AAR convention.
There were 6 filters for C100 and 5 for C200 available.
Table 2.7 gives a list of these filters
including the reference and central wavelength, the widths, their
resolution and the transmission. Section 2.9 gives
more details about the calculation
of ,
and
.
Filter | ![]() |
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[![]() |
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[![]() |
||
C100 | |||||
C50 | 65 | 68.7 | 60.8 | 0.04 | 42 |
C60 | 60 | 61.8 | 24.6 | 0.13 | 50 |
C70 | 80 | 80.7 | 48.4 | 0.12 | 59 |
C90 | 90 | 95.2 | 56.4 | 0.30 | 76 |
C100 | 100 | 102.6 | 47.1 | 0.27 | 84 |
C105 | 105 | 107.2 | 38.4 | 0.24 | 88 |
C200 | |||||
C120 | 120 | 118.7 | 49.5 | 0.13 | 101 |
C135 | 150 | 155.1 | 81.2 | 0.26 | 113 |
C160 | 170 | 174.3 | 89.9 | 0.43 | 134 |
C180 | 180 | 181.0 | 68.8 | 0.33 | 151 |
C200 | 200 | 202.1 | 56.9 | 0.22 | 168 |
PHT-S consisted of a dual grating spectrometer with resolving power of
order 90 in two wavelength bands. Band SS
covered the wavelength range 2.5-4.9 m and band
SL
covered the range 5.8-11.6
m.
Each spectrometer used a linear array of 64 element Si:Ga detectors
with dimensions of
mm
per element.
The arrays, hence the dispersion direction, were oriented in the spacecraft
Z-direction. PHT-S had one square entrance aperture with dimensions
; this aperture was imaged onto each detector pixel.
In dispersion direction this resulted
in a triangular spectral bandpass with a spectral range
(Full Width at Half Maximum) for a single detector
of 42.4nm (=3500 kms) for PHT-SS and 96.6nm
(=3200 kms
) for PHT-SL. The resolution was about 85
for PHT-SS and about 95 for PHT-SL, respectively.
The spectra could be fully sampled at half of the resolution, i.e. with 89nm (PHT-SS) and 189.8nm (PHT-SL).
PHT-S could be used with the chopper.
Both gratings were operated in first order. The wavelength scale was established in-orbit against celestial sources which emit narrow lines by fitting a 2nd order polynomial through the measured line centers.