XRCF HRMA On-axis Effective Area

XRCF HRMA On-axis Effective Area

Ping Zhao

Smithsonian Astrophysical Observatory

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

August 9, 2000



Introduction

NASA's Chandra X-ray Observatory (CXO) was successfully launched on July 23, 1999 by the space shuttle Columbia. It has returned fruitful scientific results in the past year. CXO has unprecedented capabilities of high resolution imaging and spectroscopy over the X-ray energy band of 0.1 keV - 10 keV. The effective area of its X-ray mirror - High-Resolution Mirror Assembly (HRMA) - was measured using the X-Ray Calibration Facility (XRCF) at the Marshall Space Flight Center (MSFC) in Huntsville, AL from late 1996 to early 1997.

Immediately after the XRCF HRMA calibration, it was found that there were substantial discrepancies between the experimental results and the predicted effective area based on the raytrace simulations according to the HRMA model at that time. The calibration data show that, for energies higher than 2 keV, the measured effective area was less than the predicted effective area by 10%, which is beyond the experimental errors.

During the period from late 1998 to early 1999, improvements were made in the SAOSAC raytrace model and the discrepancies were reduced to about 5%. In early 2000, more improvements were made in the optical constant used to calculate the mirror reflectivity. This has made the measured effective area agree reasonably well with the raytrace simulation for shells 3, 4 and 6. Although there is still a large discrepancy for shell 1. However, the agreement is very good for the assembly - HRMA. Using the XRCF measurements to calibrate the raytrace simulations, here are the predictions of the HRMA on-axis effective area for both at XRCF and on-orbit.


SAOSAC Raytrace Simulations and Calibration Results

The SAOSAC raytrace simulations were generated from the HRMA model which is based on measurements of HDOS metrology, Kodak assembly and the XRCF X-ray test. Its trace-shell configuration file can be found here.

The key raytrace configurations are:

There are three kinds of XRCF calibration measurement of the HRMA on-axis effective area:
  • X-ray spectral line measurements with the Flow Proportional Counter (FPC).
  • X-ray spectral line measurements with the Solid State Detector (SSD).
  • X-ray carbon continuum measurements with the Solid State Detector (SSD). Here are the comparisons of the XRCF HRMA on-axis effective area between the measurements and the raytrace simulations with a 2mm diameter aperture, which was the largest aperture used with the SSD measurements: The top panels show the raytrace simulations (generated by Diab Jerius), spectral line FPC and SSD data (analyzed by Richard Edgar) and C-continuum SSD data (analyzed by Ping Zhao). The bottom panels show the ratio of measurement/simulation. A polynomial was fit to each of the ratio curve.


    XRCF HRMA On-axis Effective Area

    The XRCF HRMA On-axis Effective Area, as well as the On-orbit HRMA On-axis Effective Area, were generated by multiplying the raytrace simulations with the XRCF calibration data scaling factors.

    The XRCF calibration data scaling factors are:
    Here are the results of XRCF HRMA On-axis Effective Area:
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