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Calculation without Gratings

The AXAF telescope mirrors consist of four shells of zerodur coated with 350 /AA of iridium that reflect electromagnetic radiation at grazing incidence angles of about 0.44 degrees to 0.84 degrees. The mirrors are constructed in such a way as to present concentric annuli to incoming radiation. The dimensions of the four annuli are given in the following table (van Speybroeck, private communication).
 


Table C.1: AXAF Mirror Parameters 
Mirror Number Front Radius (mm) Back Radius (mm)
1 612.69 600.34
3 493.41 483.47
4 435.63 426.85
6 323.82 317.29

In order to compute the intensity of optical light for an on-axis source, the Airy function for each mirror was computed at two wavelengths: 450 nm and 850 nm, corresponding to the peak transmission wavelengths of the optical blocking filters. The reflectivity in the optical band at these grazing angles of incidence is very high, $\sim$99%, based on the optical constants found by Weaver (1977). The contributions to the Airy function from each mirror annulus were added incoherently, as no effort was made during fabrication to align the mirrors to the accuracy necessary to maintain coherence. An example of the results of the calculation for the two wavelengths is shown in Figures C.1, C.2, and C.3. The fraction of the encircled energy for the pixel at the on-axis point was taken to be 0.03 and 0.06 at 850 nm and 450 nm respectively. In the integration over the bandpass carried out to compute the optical fraction transmitted, OF (see Equation 5.18), the encircled energy was computed at a number of wavelengths and interpolated linearly with wavelength.

The encircled energy is included in the term Atel($\lambda$).

Figure C.1 shows the point spread function of the telescope computed at 450 nm. The small `dips' are interference effects. This curve was multiplied by , where  is the off-axis angle variable of integration and integrated to a specific off-axis angle to produce the results shown in Figure C.2. The same procedure was used to produce the results at 850 nm, shown in Figure C.3.
 
 

Figure C.1:  The point spread function of the AXAF mirrors at 450 nm as a function of off-axis angle in arc seconds.

 
 

Figure C.2:  The encircled energy as a function of off-axis angle for the AXAF mirrors at 450 nm.

 
 

Figure C.3:  The encircled energy as a function of off-axis angle for the AXAF mirrors at 850 nm.


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