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X-Ray Testing Constellation-X Optics at MSFC's 100-m FacilityIn addition to the 530-m-long X-Ray Calibration Facility (XRCF), NASA's Marshall Space Flight Center (MSFC) operates a 104-m-long (source-to-detector) X-ray-test facility. Originally developed and still occasionally used for stray-light testing of visible-fight optical systems, the so-called "Stray-Light Facility" now serves primarily as a convenient and inexpensive facility for performance evaluation and calibration of X-ray optics and detectors. The facility can accommodate X-ray optics up to about 1-m diameter and 12-m focal length. Currently available electron-impact sources at the facility span the approximate energy range 0.2 to 100 keV, thus supporting testing of soft- and hard-X-ray optics and detectors. Available MSFC detectors are a front-illuminated CCD (charge-coupled device) and a scanning CZT (cadmium--zinc--telluride) detector, with low-energy cut-offs of about 0.8 and 3 keV, respectively. In order to test developmental optics for the Constellation-X Project, led by NASA's Goddard Space Flight Center (GSFC), MSFC undertook several enhancements to the facility. Foremost among these was development and fabrication of a five-degree-of-freedom (5-DoF) optics mount and control system, which translates and tilts the user-provided mirror assembly suspended from its interface plate. Initial Constellation-X tests characterize the performance of the Optical Alignment Pathfinder Two (OAP2) for the large Spectroscopy X-ray Telescope (SXT) and of demonstration mirror assemblies for the Hard X-ray Telescope (HXT). With the Centroid Detector Assembly (CDA), used for precision alignment of the Chandra (nee AXAF) mirrors, the Constellation-X SXT Team optically aligned the individual mirrors of the OAPZ at GSFC. The team then developed set-up and alignment procedures, including transfer of the alignment from the optical alignment facility at GSFC to the X-ray test facility at MSFC, using a reference flat and fiducials. The OAPZ incorporates additional ancillary features --- fixed aperture mask and movable sub-aperture mask --- to facilitate X-ray characterization of the optics. Although the OAPZ was designed to- have low sensitivity to temperature offsets and gradients, analyses showed the necessity of active temperature control for the X-ray performance testing. Thus, the Smithsonian Astrophysical Observatory (SAO) implemented a thermal control and monitoring system, designed to hold the OAP2 close to its assembly.
Document ID
20030068234
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
O'Dell, Stephen
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Baker, Markus
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Content, David
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Freeman, Mark
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Glenn, Paul
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gubarev, Mikhail
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hair, Jason
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Jones, William
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Joy, Marshall
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Optics
Meeting Information
Meeting: Optics for EUV, X-Ray, and Gamma-Ray Astronomy
Location: San Diego, CA
Country: United States
Start Date: August 3, 2003
End Date: August 8, 2003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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