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Flight Mirror Assembly

The next-generation astronomical X-ray telescopes, such as IXO, require extremely large collecting area combined with good angular resolution and high area-to-mass ratio in order to achieve unprecedented sensitivities for the study of the high-z Universe and for high-precision spectroscopy of bright X-ray sources.

The Flight Mirror Assembly (FMA) provides an effective area of 3 m 2 at 1.25 keV, 0.65 m 2 at 6 keV, and 150 cm 2 at 30 keV. To meet the observatory's 5 arcsec half-power diameter (HPD) requirement, the FMA angular resolution must be 4 arcsec for E < 7 keV and 30 arcsec at 30 keV. Attaining the large effective area within the launch vehicle mass constraint requires a mirror with a high area-to-mass ratio: 20 cm 2/ kg, which is 50 times larger than Chandra and eight times larger than XMM-Newton.

The FMA uses the nested grazing incidence mirrors to focus X-ray photons on the detector plane. The challenge has been to develop a technique to produce mirrors rapidly with the characteristics to fulfill the IXO angular resolution requirement. A key feature of the IXO mirror design is a single mirror assembly that is optimized to minimize mass while maximizing the collecting area.

Two X-ray mirror technology options are in development for IXO: segmented glass (with development led by NASA) and silicon micro-pore optics (with development led by ESA). Both methods are making very good progress, and are described in more detail below, see Segmented Glass Optics and Silicon Pore Optics. With either of these technologies, the IXO mirrors will meet or exceed performance requirements.

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Segmented Glass Optics

Illustration of the segmented glass technique under development 
    by the GSFC mirror development lab

Illustration of the glass slumping technique under development by the GSFC mirror development lab

Photo of a single glass segment shaped by the glass slumping 

Photo of a single glass segment shaped by the glass slumping technique

The segmented glass optics are being developed at the Goddard Space Flight Center (GSFC) mirror development lab. The mirror team has worked over the past decade perfecting a new technique to produce high-quality mirror segments rapidly. The mirror production begins with commercially-available glass and a properly figured and polished mandrel (rounded mold) with the required shape for the final mirror segment. The glass segment is placed on the mandrel and then in an oven. As the oven heats up to about 600° C, the glass softens and sags under its own weight, wrapping itself around the mandrel. When the glass is removed the resulting segment is a perfect replication of the mandrel's surface.

Two recent developments have proven that this glass segmenting technique is ready for prime time. In early 2008, the FMA technology team tested a two-mirror system and achieved an angular resolution of 14.7 arcsec at 8 keV, proving that the requirements of IXO are all but certain to be met by the segmented glass mirror segments. In addition, the GSFC mirror lab has been enlisted to produce the over 3000 mirror segments for the NuSTAR (Nuclear Spectroscopic Telescope Array) mission. NuSTAR is a SMEX mission planned for launch in 2011.

For more information, refer to

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Silicon Pore Optics

The Silicon Pore Optics is a European technology developed on the basis of commercially available silicon wafers from the semiconductor industry. This is novel technology for producing very light, stiff and modular X-ray optics that can be assembled into almost arbitrarily large apertures—and therefore are perfectly suited for IXO. As starting material, the Silicon Pore technology uses silicon wafers from the semiconductor industry. The wafers are then stacked into a pore structure with concentric cylindrical surfaces.

The wafers are bent into an accurate cone and assembled to form a light and stiff pore structure with pores of the order of a millimeter in size. The resulting modules form a small segment of a Wolter-I optic and are easily assembled into an optic with large collecting area. Hundreds of such mirror modules are finally integrated into petals, and mounted onto the spacecraft to form an X-ray optic of several meters in diameter. Read more ...

Illustration of the mirror assembly for the IXO silicon pore optics

Photographs credit of ESA, Cosine Research, Kayser-Threde, Micronit, SRON,NSI and MPE.

For more information, refer to

  • Collon, M. J. et al., 2008, Proc. of SPIE Vol. 7011, 70111E
Read more about silicon pore optics on the ESA web site Read more

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Selected References

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