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Subsections


A.1 Mean Filter/Aperture Specifications  

A.1.1 PHT-P Filters  

The PHT-P filters are located on Change Wheel III (CHW3). Each wheel position is indicated by an integer. In the following table the filter specifications corresponding to a Change Wheel III position have been listed. The values for the spectral resolution (${\lambda}_c/{\Delta}{\lambda}$) and airy diameter (dAiry) have been measured in laboratory. The system responses (Rmean) have been derived from in-flight data. The reference central wavelength (${\lambda}_{ref}$) is defined as a wavelength close to the isophotal centre of the filter, and where possible, matching values given for filters corresponding to other ISO and IRAS instruments (see [20]).


 
Table A.1: Description of the PHT-P filters on CHWIII
Wheel  Filter  ${\lambda}_{ref}$  ${\lambda}_c/{\Delta}{\lambda}$  Rmean  dAiry  description                   
position   ID (${\mu}m$)     ('')  
1 P1_3p29_UM 3.3 15.160 0.103 2.8 PAH
2 P1_3p6_UM 3.6 3.620 0.127 3.0 Cosmological gap, cf ISOCAM
3 P1_4p85_UM 4.8 3.140 0.152 4.1 Continuum
4 P1_7p3_UM 7.3 2.190 0.212 6.2 Continuum
5 P1_7p7_UM 7.7 9.320 0.194 6.4 PAH
6 P1_10_UM 10 5.551 0.177 8.4 sillicate feature
7 P1_11p3_UM 11.3 14.070 0.177 9.5 PAH
8 P1_12p8_UM 12.8 5.330 0.089 10.8 Continuum
9 P1_16p0_UM 15 1.820 0.130 13.8 Continuum
10 P1_11p5_UM 12 5.550 0.156 10.0 IRAS 12 ${\mu}m$ cf. ISOCAM
11 P2_20_UM 21.03 2.330 0.324 17.7 Close to Q band
12 P2_25_UM 25 2.610 0.370 20.0 IRAS 25 ${\mu}m$
13 P3_60_UM 60 2.350 0.111 50.3 IRAS 60
14 P4_100_UM 100 2.590 0.303 83.9 IRAS 100

A.1.2 PHT-P Apertures  

The PHT-P apertures are located on the inner circle of Change Wheel II (CHW2). Each wheel position is indicated by an integer. In the following table the aperture specifications corresponding to a Change Wheel II position have been listed.


 
Table A.2: Description of the PHT-P apertures located on CHWII
Wheel  Aperture  Diameter  Area  Solid Angle  description                   
position   ID ('') (mm2) (10-8 ster)  
1 52_SEC 52 4.1548 5.13 circular 2.3 mm
2 79_SEC 79 9.0792 11.21 circular 3.4 mm
3 99_SEC 99 14.522 17.93 circular
4 120_SEC 120 21.237 26.22 circular
5 127$\times$127_SEC 127$\times$127 30.250 37.3 square
6 180_SEC 180 48.398 59.8 circular
7 180_SEC_XBLK       not used
8 5_SEC 5 0.0314 0.039 circular
9 7p6_SEC 7.6 0.1001 0.124 circular
10 10_SEC 10 0.1735 0.214 circular
11 13p8_SEC 13.8 0.2827 0.349 circular
12 18_SEC 18 0.5218 0.625 circular
13 20$\times$32_SEC 20$\times$32 1.1288 1.39 rectangular
14 23_SEC 23 0.7854 0.97 circular

A.1.3 PHT-C Filters  

The PHT-C filters are located in the outer circle of Change Wheel II (CHW2). In the following table the filter specifications corresponding to a Change Wheel II position have been listed. The values for the spectral resolution (${\lambda}_c/{\Delta}{\lambda}$) and point spread function factor (fpsf) have been measured in laboratory. The system responses (Rmean) have been derived from in-flight data. The reference wavelength (${\lambda}_{ref}$) is defined as a wavelength close to the isophotal centre of the filter, and where possible, matching values are given for filters corresponding to other ISO and IRAS instruments (see [20]).

The point spread function factor represents the fraction of the power in the beam falling on the whole detector array if the beam is centered on the array (the values have been derived from in-flight data, see section 9 for an explanation). The geometrical solid angles of the pixels are slightly filter dependent, their averages are:


${\Omega}_{C100}$ = 0.0688${\times}10^{-6}$ sr
${\Omega}_{C200}$ = 0.281${\times}10^{-6}$ sr


 
Table A.3: Description of the PHT-C filters on CHWII
Wheel  Filter  ${\lambda}_{ref}$  ${\lambda}_c/{\Delta}{\lambda}$  Rmean  fpsf  description                   
position   ID (${\mu}m$)     ('')  
1 C100_OPEN         not used
2 C100_90_RED 90 1.730 0.296 0.900 wide band cont.(backup)
3 C100_50_UM 65 1.130 0.045 0.912 continuum
4 C100_60_UM 60 2.510 0.130 0.918 continuum IRAS 60 ${\mu}m$
5 C100_70_UM 80 1.670 0.121 0.902 continuum
6 C100_100_UM 100 2.180 0.270 0.892 continuum IRAS 100 ${\mu}m$
7 C100_105_UM 105 2.790 0.236 0.884 continuum
8 C100_90_UM 90 1.690 0.296 0.900 wide band continuum
9 C200_160_UM 170 1.940 0.431 0.708 wide band continuum
10 C200_200_UM 200 3.550 0.215 1.054 continuum
11 C200_180_UM 180 2.630 0.327 0.972 continuum
12 C200_135_UM 150 1.910 0.260 0.668 continuum
13 C200_120_UM 120 2.400 0.131 0.574 continuum
14 C200_RETICLE 0.00 0.00 0.00 0.00 not used

A.1.4 Other Filterwheel Components  

Change Wheel I (CHW1) is either used to redirect the light to the next optical component such as PHT-S, the inner Change Wheel II and the outer Change Wheel II, or is used to put a polariser in the beam. In the following table the specifications corresponding to a Change Wheel I position have been listed.  

 
Table A.4: Description of CHWI
Wheel  Element  description                     
position   ID    
1 PHT_P_POL000 PHT P Polariser $0{\deg}$  
2 PHT_P_POL120 PHT P Polariser $120{\deg}$  
3 PHT_P_POL240 PHT P Polariser $240{\deg}$  
4 PHT_P_NO_POL PHT P Flat mirror  
5 PHT_S PHT S Flat mirror  
6 PHT_C_RETICL PHT C C-cut Quartz  
7 PHT_C_FREE1 PHT C Free aperture  
8 PHT_C_FREE2 PHT C Free aperture  
9 PHT_C_FREE3 PHT C Free aperture  
10 PHT_S_REDUND PHT S Flat mirror (redundant)  
11 PHT_C_POL000 PHT C Polariser $0{\deg}$  
12 PHT_C_POL120 PHT C Polariser $120{\deg}$  
13 PHT_C_POL240 PHT C Polariser $240{\deg}$  
14 PHT_C_NO_POL PHT C Free aperture  


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Next: A.2 Filter Transmission Data Up: A Instrument Tables Previous: A Instrument Tables

ISOPHOT Data Users Manual, Version 4.1, SAI/95-220/Dc