HRMA On-orbit Focal Length

HRMA On-orbit Focal Length

Ping Zhao

Smithsonian Astrophysical Observatory

zhao@cfa.harvard.edu, 617-496-7582

August 8, 2000



Definition

For a point source of infinite distance with a small offaxis angle, theta, its image is projected to the focal plane (a flat plane perpendicular to and intersect with the optical axis at the onaxis focus) at a distance r from the onaxis focus. The HRMA On-orbit Focal Length (FL) is defined as:
 
		FL = r/tan(theta) 

The designed HRMA On-orbit Focal Length (for an ideal HRMA) is: 

		FL(ideal) = 10065.54532 mm 

Estimates based on on-ground measurements

For the real HRMA, there was no direct measurement of its On-orbit Focal Length possible before launch. However, there were six different estimates of the absolute distance between the HRMA On-orbit focus to the front surface (paraboloid side) of the Central Aperture Plate (CAP Datum A), based on several independent direct measurements during various stages of the Chandra development. They are:
Source of estimate			   HRMA focus to Datum A (mm)
---------------------------------------------------------------------
Kodak from ATP & ARM data [1]				10079.5
SAO from ATP & ARM data [2]				10079.4	 
TRW from XRCF data (measurement 1) [3]			10079.1  
TRW from XRCF data (measurement 2) [3]			10080.2  
TRW from FACT data (measurement 1) [4]			10081.9
TRW from FACT data (measurement 2) [4]			10079.5
---------------------------------------------------------------------
	    			     Average 		10079.93
				     Standard deviation     1.03

ATP & ARM: HRMA Acceptance Test Procedure & Factory Alignment Reference Mirror. 
XRCF: Cross check using the laser rangefinder done at the XRCF.
FACT: Focus Alignment Cross-Check done at the observatory level at TRW.

References:

  • 1. Email from Atkinson/Kodak dated 12 Aug 1997.
  • 2. Memo by Podgorski & Gaetz/SAO dated 29 Aug 1997.
  • 3. Email from Texter/TRW dated 17 Apr 1997.
  • 4. Email from Podgorski/SAO dated 10 Feb 1998.

    This gives a good estimate of the absolute distance between the HRMA focus to the CAP Datum A, and a good estimate of the uncertainty, which is about one millimeter.


    SAOSAC Raytrace Calculation

    Meantime, SAOSAC raytrace (with focus turned on, hence the scattering is turned off) gives the distance between the HRMA focus to the CAP Datum A to be 10079.772 mm, which differs only 0.17 mm from the average of the above measurements and well within the measurement errors. This is very important since the SAOSAC is build around the HRMA model based on the HDOS metrology, Kodak assembly and the XRCF X-ray test data; and it is completely independent of the above absolute measurements of the HRMA focus to Datum A distance. This indicates that the current HRMA model in SAOSAC is a faithful representation of the real HRMA regarding the focal length.

    Therefore the HRMA On-orbit Focal Length can be calculated with good faith using the SAOSAC. Figure 1 illustrates the method of this calculation. Rays from onaxis source come in parallel to the HRMA optical axis and are focused at the onaxis focal point F. The Focal Plane is a flat plane intersect with the optical axis at F. (Detector HRC-I is placed in this plane.) Rays from a offaxis source come in with a small angle theta from the optical axis and are focused on a curved surface between the Focal Plane and the HRMA. The HRMA Focal Length is the distance between points O and F on the optical axis. However, the position of O is unknown. In SAOSAC, the Z-axis is the optical axis and the CAP Datum A is at Z = 0.



    postscript

    For onaxis and offaxis sources, SAOSAC calculates coordinates of the best focal positions as (xo,yo,zo) and (x,y,z) (see Figure 1).
    	Let r' = sqrt[(x-xo)^2 + (y-yo)^2]
    	    FL = r'/tan(theta) + zo - z	
    
    This way the FL can be calculated using SAOSAC, for different energies and offaxis angles.


    Results

    Figures 2-7 show the results of these calculations for 6 energies ( 0.277, 1.497, 4.511, 6.404, 8.639, and 9.700 keV), 8 offaxis angles (1, 2, 3, 5, 7, 10, 15, 20 arcmin) and 4 azimuthal angles (0, 90, 180, 270 degree). Figure 8 is a colored summary plot of the results. The dotted line in the figure is the designed HRMA Focal Length and Plate Scale.

    It is seen that the HRMA FL is a function of energy and offaxis angle. And it is also slightly asymmetric azimuthally.

    Table 1 shows the HRMA On-orbit Focal Length averaged for each energy within certain radii of offaxis angles.


    Table 1. Average HRMA On-orbit Focal Length (mm) Energy Offaxis angle within radius of (arcmin) (keV) 3 5 10 15 20 --------------------------------------------------------------- 0.2770 10069.782 10069.571 10069.164 10068.902 10068.563 0.463 0.571 0.787 0.988 1.303 1.4967 10069.737 10069.524 10069.116 10068.852 10068.509 0.463 0.573 0.790 0.994 1.313 4.5108 10068.465 10068.228 10067.723 10067.336 10066.773 0.470 0.621 0.957 1.334 1.982 6.4038 10065.213 10064.884 10064.154 10063.685 10063.064 0.688 0.965 1.506 1.874 2.460 8.6389 10063.697 10063.280 10062.373 10061.872 10061.308 0.938 1.318 2.162 2.472 2.837 9.7000 10063.219 10062.760 10061.841 10061.253 10060.722 3.145 3.419 3.600 3.722 3.820 --------------------------------------------------------------- Mean 10066.685 10066.374 10065.728 10065.316 10064.823 Error 3.079 3.254 3.601 3.813 4.063 ---------------------------------------------------------------
    For a near axis (theta =< 3 arcmin) soft source (E < 2 keV), the HRMA Focal Length = 10069.760 +/- 0.454 mm. Considering the systematic error of 1mm from the direct on-ground measurements. We have:
    	HRMA On-orbit Focal Length = 10069.8 +/- 1.1 mm
    
    	HRMA Near Axis Plate Scale = 48.8196 +/- 0.0053 micron/arcsec
    

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