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Proceedings Paper

High resolution and high throughput x-ray optics for future astronomical missions
Author(s): W. W. Zhang; M. P. Biskach; P. N. Blake; V. T. Bly; J. M. Carter; K. W. Chan; J. A. Gaskin; M. Hong; B. R. Hohl; W. D. Jones; J. J. Kolodziejczak; L. D. Kolos; J. R. Mazzarella; R. S. McClelland; K. P. McKeon; T. M. Miller; S. L. O'Dell; R. E. Riveros; T. T. Saha; M. J. Schofield; M. V. Sharpe; H. C. Smith
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Paper Abstract

X-ray optics is an essential component of every conceivable future x-ray observatory. Its astronomical utility is measured with two quantities: angular resolution and photon collecting area. The angular resolution determines the quality of its images and the photon collecting area determines the faintest sources it is capable of detecting and studying. Since it must be space-borne, the resources necessary to realize an x-ray mirror assembly, such as mass and volume, are at a premium. In this paper we report on a technology development program designed to advance four metrics that measure the capability of an x-ray mirror technology: (1) angular resolution, (2) mass per unit photon collecting area, (3) volume per unit photon collecting area, and (4) production cost per unit photon collecting area.

We have adopted two approaches. The first approach uses the thermal slumping of thin glass sheets. It has advantages in mass, volume, and cost. The objective for this approach is improving its angular resolution. As of August 2013, we have been able to consistently build and test with x-ray beams modules that contain three co-aligned Wolter-I parabolichyperbolic mirror pairs, achieving a point spread function (PSF) of 11 arc-second half-power diameter (HPD), to be compared with the 17 arc-seconds we reported last year. If gravity distortion during x-ray tests is removed, these images would have a resolution of 9 arc-seconds, meeting requirements for a 10 arc-second flight mirror assembly. These modules have been subjected to a series of vibration, acoustic, and thermal vacuum tests.

The second approach is polishing and light-weighting single crystal silicon, a material that is commercially available, inexpensive, and without internal stress. This approach has advantages in angular resolution, mass, and volume, and objective is reducing fabrication cost to make it financially feasible to fabricate the ~103 m2 mirror area that would be required for a future major x-ray observatory.

The overall objective of this technology program is to enable missions in the upcoming years with a 10 arc-second angular resolution, and missions with ~1 arc-second angular resolution in the 2020s.


Paper Details

Date Published: 26 September 2013
PDF: 13 pages
Proc. SPIE 8861, Optics for EUV, X-Ray, and Gamma-Ray Astronomy VI, 88610N (26 September 2013); doi: 10.1117/12.2024250
Show Author Affiliations
W. W. Zhang, NASA Goddard Space Flight Ctr. (United States)
M. P. Biskach, Stinger Ghaffarian Technologies, Inc. (United States)
P. N. Blake, NASA Goddard Space Flight Ctr. (United States)
V. T. Bly, NASA Goddard Space Flight Ctr. (United States)
J. M. Carter, NASA Marshall Space Flight Ctr. (United States)
K. W. Chan, Univ. of Maryland, Baltimore County (United States)
J. A. Gaskin, NASA Marshall Space Flight Ctr. (United States)
M. Hong, Stinger Ghaffarian Technologies, Inc. (United States)
B. R. Hohl, Stinger Ghaffarian Technologies, Inc. (United States)
W. D. Jones, NASA Marshall Space Flight Ctr. (United States)
J. J. Kolodziejczak, NASA Marshall Space Flight Ctr. (United States)
L. D. Kolos, NASA Goddard Space Flight Ctr. (United States)
J. R. Mazzarella, Stinger Ghaffarian Technologies, Inc. (United States)
R. S. McClelland, Stinger Ghaffarian Technologies, Inc. (United States)
K. P. McKeon, Stinger Ghaffarian Technologies, Inc. (United States)
T. M. Miller, NASA Goddard Space Flight Ctr. (United States)
S. L. O'Dell, NASA Marshall Space Flight Ctr. (United States)
R. E. Riveros, NASA (United States)
T. T. Saha, NASA Goddard Space Flight Ctr. (United States)
M. J. Schofield, Stinger Ghaffarian Technologies, Inc. (United States)
M. V. Sharpe, Stinger Ghaffarian Technologies, Inc. (United States)
H. C. Smith, Stinger Ghaffarian Technologies, Inc. (United States)


Published in SPIE Proceedings Vol. 8861:
Optics for EUV, X-Ray, and Gamma-Ray Astronomy VI
Stephen L. O'Dell; Giovanni Pareschi, Editor(s)

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