NASA is developing the next generation of X-ray optics that could be used in an orbiting X-Ray Observatory. The “lens” consists of thousands of mirrors positioned to reflect X-rays at a shallow angle at focal length of 3-10 meters. Locating and fixing the mirrors in position is the primary challenge of the project. Creating focus at the long focal lengths requires a mirror angular position tolerance of only 1 μRadian, and the precisely shaped mirrors, when mounted, must distort less than 0.1 μm from their free, unmounted state. Any such assembly must be able to hold these positions through launch and deployment.

Epoxy syringe and capacitive displacement sensors. The mirror is transparent at the camera angle.

The typical mirror is about the size of a sheet of printer paper and only four times as thick (200 x 200 x 0.4 mm), and is coated with a 10-nm layer of iridium or gold. Thermal expansion is also a concern; a person’s prolonged proximity to a mirror creates a measurable distortion, so the mounting process must add very little heat to the structure.

Mirrors are mounted on tabs in the final assembly and fixed in place with ultraviolet (UV)-cured epoxy. The injection and curing of the epoxy are the critical steps. The dynamics of the hydraulic pressure during and immediately after the epoxy’s injection displace the mirror at the points of contact, causing distortion and placement changes. The epoxy also expands during the UV cure process, which further distorts the mirror.

High-resolution capacitive displacement sensors from Lion Precision have been used to profile, with nanometer precision, the mirror’s displacement during the bonding process. Having profiled the movements and distortions created by the hydraulic pressure and the UV curing process, the amount of epoxy injected and the timing of the UV cure can be used to control the final mirror position. The capacitive sensors are used during the automated bonding sequence to stop the injection when the mirror distortion reaches a predetermined point. The system then monitors the mirror position during the post-injection epoxy flow. The UV curing process is begun when the mirror reaches a position from which the epoxy cure expansion will move the mirror precisely to its desired position with better than 1 μm of accuracy.

Six capacitive displacement sensors are used in the system — one for each corner of the mirror and two to monitor the mounting tab positions as a reference. Capacitive displacement sensors usually require a grounded target to prevent accumulation of charge on the target, but the fragile mirrors cannot be grounded. The sensors are designed to prevent this problem; the excitation signals have a 180° phase difference between even- and odd-numbered channels. This phase arrangement allows half of the sensors to add charge to the mirror while the other half removes charge, thereby eliminating the need for a conductive path to ground.

Elite Series high-resolution capacitive
displacement sensors
Lion Precision
St. Paul, MN

For Free Info Click Here 

NASA Tech Briefs Magazine

This article first appeared in the July, 2012 issue of NASA Tech Briefs Magazine.

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