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1.INTRODUCTIONThe availability of fast and reliable spatial light modulators (SLM) for space would allow targeting new types of applications. As an example, the aim of the EU H2020 funded SURPRISE project consists in developing a super-resolved compressive imager operating in the visible-near infrared (VNIR) and mid-wave infrared (MWIR) spectral ranges. The instrument concept is based on the use of a digital micro-mirror device (DMD) as a core element of its architecture to enable data acquisition and compression in single step based on the compressive sensing principle. In this context, the availability of a space compatible SLM active over a large spectral range will be crucial for the success of future missions possibly relying on this technology. Today, Texas Instruments benefits from a monopolistic position on the market of commercial DMDs. These devices are integrated in most of commercial video projection systems (i.e. beamers). One aim of the SURPRISE project lies in the development of a European-based solution. Nevertheless, for the SURPRISE demonstrator, a commercial component from TI has been selected. This enables reducing the development cost and initiate the development of the demonstrator prior finalizing the custom European design. Each DMD model from TI is encapsulated with a protective window made from glass with an anti-reflection coating designed for a specific spectral range. However, none of the DMD models was compatible with the required large spectral range for the SURPRISE demonstrator (VIS-NIR and MWIR). Nevertheless, without protective window, the micromirrors made of aluminum present an intrinsic reflectivity compatible with such a large spectral range. In this paper, we first present investigations performed to rework the selected DMD by replacing the original borosilicate window with an uncoated window presenting a high transmittance over the VIS-NIR and MWIR spectrum. The reworking process must be carried out safely to protect the sensitive micro-mirrors from dust and water vapor all along the process, and over the whole lifetime of the reworked DMD. Second, we present an assessment of the micro-mirror reflectivity in VNIR and MWIR spectral ranges, with and without the replacement protective window. Finally, the micro-mirror switching time and pointing stability were measured since these are key parameters in view of the future demonstration with the SURPRISE prototype. 1.1Selected commercial digital micro-mirror deviceConsidering the targeted specifications for the SURPRISE demonstrator, the model DLP7000 from TI was selected in its evaluation kit version (DLPLCR70EVM) together with a controller (DLPLCRC410EVM) to facilitate performance tests. The main optical specifications of this DMD are summarized in Table. Table 1-1.DLP7000 optical specifications.
Each micro-mirror of this DMD can be actuated independently along binary positions, either deflected at +12° or -12° with respect to the horizontal plane. 2.FRONT-WINDOW REPLACEMENT PROCEDUREAs explained above, the main challenge for integrating a commercial off-the-shelf (COTS) DMD in the SURPRISE demonstrator lies in the limited spectral transmittance range of protective windows. We thus investigated ways to remove the original window and replace it with a better-suited glass interface, without damaging the micro-mirrors. Similar reworking processes have already been reported in the literature [1][2][3]. Based on these studies, we investigated two solutions for sealing the replacing protective window: indium wire and epoxy resin. 2.1Selection of materialsSapphire was selected for replacing the protective window since this glass presents a high transmittance over a wavelength range from 400 nm to 5 μm, is characterized by a high hardness and its coefficient of thermal expansion (CTE) almost matches the metallic housing frame. The window was procured from Crystran (UK) with a diameter of 25 mm and 1 mm thickness. The aperture covers the full DMD size, and a 1 mm thickness offers a sufficient mechanical resistance to the shear stress resulting from the assembly process. The frame was manufactured in Kovar, with a CTE that matches both the sapphire window and DMD frame. 2.2Indium wire sealingA CAD model of the DMD, replacing window and frame was designed, as shown in Figure 2. Prior finalizing the designed reworking procedure, we realized a preliminary validation test of indium sealing. This test was conducted onto an existing DMD that was sealed with its package into a mechanical housing. The resulting assembly was then tested with a helium leak detector. This test proved a lack of hermiticity of the assembly. After the leak detection test, the DMD was disassembled for further inspection and confirmed a poor adhesion of the frame onto the housing. Figure 3 shows pictures of the different parts after disassembly. This first realization led to the conclusion that indium sealing was inappropriate for the following reasons: 2.3Epoxy resin sealingConsidering the results obtained with the indium wire sealing implementation, we investigated a second approach based on epoxy resin sealing. The final reworking procedure consists of the following steps:
Initial tests followed a procedure in which steps 2 and 3 were combined and performed in a clean environment but at a normal atmosphere. These units were initially functional, but were progressively deteriorated, featuring more and more non-functional pixels. Further investigation showed that the presence of oxidants such as oxygen and water vapour inside the encapsulation were the main cause of damage of the micro-mirrors flexing structures. The procedure had to be adapted to perform the encapsulation inside an inert or oxidant-free atmosphere such as nitrogen or any inert gas. Due to equipment availability, the aforementioned solution using a glovebox and argon was selected showing good results. Unfortunately, the stability of the solution was not sufficient, as eight days after encapsulation the micro-mirrors started showing the same problems. The final modification in the procedure to guarantee a longer-term hermicity of the encapsulation, the parylene deposition, proved to be sufficient, as at the time of writing, the reworked units are fully functional after 10 months. This method allows obtaining a highly hermetic package and facilitates the development of a reliable and repeatable process that fulfils the application requirements. 3.PERFORMANCES CHARACTERIZATIONOnce the reworking procedure validated, we could prepare reworked DMDs fulfilling the requirements in terms of spectral range and reliability. The reflectivity of micro-mirrors was characterized both with the replacement front window and without, to ensure its compatibility with the SURPRISE demonstrator. In parallel, operation verification tests were performed before and after the replacement of the front window to ensure a nominal functionality after rework. In addition, the micro-mirror switching time and pointing direction stability were evaluated on an original DMD. These characteristics are key for a successful demonstration of the SURPRISE concept. 3.1Visible spectrum transmissionThe aim was to measure the spectral reflectivity of micro-mirrors in the wavelength range 400-2000 nm both with the new sapphire front window and without. The test was carried out using Agilent Technologies’ Cary 7000 UV-Vis-NIR Spectrophotometer, including Cary Universal Measurement Accessory (UMA) for reflectivity measurement. The characterization was performed with micro-mirrors in off-state. The resulting reflectivity in VNIR range of all both samples is depicted in Figure 7. Interestingly, different incidence angles and polarization states do not greatly affect the reflectivity of both samples. No considerable impact in the reflectivity is seen between the samples with and without sapphire window. 3.2Mid-infrared spectrum transmissionThe aim was to measure the spectral reflectivity of micro-mirrors in the wavelength range 2-5 μm both with the new sapphire front window and without. The reflectivity assessment was performed using Bruker’s Vertex 70 FT-IR Spectrometer with Bruker’s HYPERION FT-IR Microscope. Measurements are performed against a reference sample made from an uncoated gold mirror. Results are presented in Figure 8. Firstly, it is worth noting that it was not possible to avoid the absorption of H2O and CO2 at certain wavelengths, due to the necessity of transmitting the light beam in the open atmosphere. For this reason, raw measurements were post-process to minimise this impact, by down sampling the signal at those specific ranges. As reference, the reflectivity using the raw signals is included as dashed lines. The reflectivity of the reworked DMD features a considerable drop above 4 μm and is considerably influenced by the polarization state. This drop matches very well the expected transmission curve of sapphire. On the other hand, micromirrors without window show a constant reflectivity in the studied spectral range, as expected for aluminium. 3.3Switching timeThe objective of this test was to measure the switching time of a small set of micro-mirror pixels from ON to OFF positions and vice versa. Then, perform a statistical analysis over several random regions of the DMD. This test aimed at verifying the maximal achievable frame rate. Figure 9 presents the assembled test setup. A focused light source illuminates a small area of the DMD where all pixels are switched from ON to OFF states and vice versa. Two optical lenses collect the reflected light onto two different photodiodes (PD), either when in ON state (PD1) or in OFF state (PD2). An oscilloscope records the signals arising from both photodiodes. Repeated several times, a statistical analysis of the switching time is performed. Since the DMD is mounted on a x-y translation stage, statistical analysis over several areas can be performed. Results were obtained for 6 random positions on the active part of the DMD. For each position, 10 measurements were recorded during the switch from one state to the other. Figure 10 plots the results for a single position showing the mean and standard deviation of the switching time for all repetitions. It is first worth noting that as the photodiodes are not the same model, some differences are appreciable in the output data from each one. Mainly, PD2 features a lower output gain leading to a smaller signal-to-noise ratio. Nevertheless, this difference does play any role on the analysis. The signal from both PDs is simultaneously sampled at 0.5 GHz and triggered by either rising edge of PD1 or PD2. The logged data is then normalised to force low and high states at 0 and 1, respectively. The transition from one state to the other is defined at 0.5 threshold. Due to lower magnitude of PD2 signal, greater sensitivity to small misalignments is experienced, generating over and undershoots of the signal. As the shape and length of such characteristics are fully determined by the alignment, they are assumed to happen at high level, and not during transition. To summarise, considering all measurements, the mean and standard deviation values of the switching time were measured as 2.99 and 0.05 μs. This short switching time ensures achieving the maximum frame rate of 32’552 Hz (30.72 μs) stated in the DLP7000 datasheet and presents a high stability. 3.4Pointing stabilityThe objective of this test was to measure the pointing direction repeatability and deviation for a single micro-mirror pixel. Then, perform a statistical analysis over several random pixels of the DMD. This test aimed at assessing the necessary alignment precision and compatibility with the SURPRISE demonstrator design. Figure 11 presents the assembled test setup. A collimated light source illuminates the DMD where all pixels are in OFF state. A single mirror on the optical axis of the detection system is then turned ON and OFF and one image is recorded to measure the reflection position on a camera, each time the mirror is turned ON, after stabilisation. By placing a camera (detector only, no lens) at a certain distance, computing the centroid of the recorded pattern enables resolving micro-mirror angle variations below 0.1°. The angular resolution will be given by the distance from the mirror to the camera, the pixel size and the precision in computing the centroid. The camera is located at approximately 45 mm from the DMD, considering a camera pixel size of 2.74 μm, an angular resolution of 0.0035° is achieved. Since the DMD is mounted on a XYZ translation stage, statistical analysis over several pixels can be performed. Results were obtained for 6 random single micro-mirror on the active part of the DMD. For each pixel, 6 repetitions were recorded. For each image, as shown for a single pixel and two repetitions in Figure 12, a gaussian distribution is fitted for both X and Y positions, giving the centre (mean μ) and width (standard deviation σ) of the light intensity. To summarise, considering all measurements, the standard deviation of the angle was measured to be inferior to 0.025°. 4.CONCLUSIONIn this report, we first investigated two ways to replace the front window of the DMD in a safe and reliable manner. The aim of this reworking process was to produce a modified DMD that fulfils the requirements in terms of spectral transmittance range for the SURPRIRSE demonstrator. The main challenge was to encapsulate the micro-mirrors in an inert atmosphere and ensure long-term hermeticity. The established procedure was then detailed and followed to assemble two SLM demonstrators. One of these demonstrators is currently being integrated into the SURPRISE demonstrator in the next steps of the project. Thanks to the characterization of micro-mirrors reflectivity with the replacement protective window and without, we could prove the compatibility of the reworked DMD with the large spectral range aimed by the SURPRISE demonstrator. Also, these spectral reflectance measurements confirmed the need for the reworking procedure and replacement of the front window with sapphire. In addition, tests on switching time and pointing stability allowed verifying the adequacy of key performances with the datasheet, which is promising in view of the future integration into the demonstrator. ACKNOWLEDGEMENTThis work is part of the SURPRISE project receiving funding from the European Union’s Horizon 2020 research and innovation programme under Grant Agreement No 870390. The authors would like to thank the invaluable support provided by Frédéric Zamkotsian from the Astrophysics Laboratory of Marseille (LAM), France, to identify the original reworking procedure limitations, and Edith Laux from the HE-Arc in La Chaux-de-Fonds, Switzerland, for sharing her expertise and facilities for the parylene deposition. We also thank the SURPRISE project team for their valuable inputs and help with the current work. REFERENCESTravinsky, Anton,
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