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EPAPS Supplementary Material An Energy-Based Model to Predict Wear in Nanocrystalline Diamond AFM Tips R. Agrawal, N. Moldovan, H. D. Espinosa* Department of Mechanical Engineering, Northwestern University, 2145 Sheridan Road, Evanston, IL 60208-3111 *corresponding author Currently at Advanced Diamond Technologies, Inc., Romeoville, IL 60466 1. Mathematical method (MM) to estimate tip radius based on surface roughness measurements A mathematical algorithm developed by Villarrubia [1] was used for de-convolution of tip radii. A 2.5 X 2.5 m2 area on the UNCD surface was characterized in terms of roughness and a calibration curve was obtained. This calibration curve relates the roughness of the “characterized surface” as measured from an AFM image, to the radius of the tip used to scan the surface. The details of the method follow. To accurately determine the surface morphology of the substrate, a sharp Silicon Nitride (Si3N4) probe (tip radius < 10 nm, as specified by the vendor (Budget sensor Inc.)) was first characterized. The tip was examined under SEM to obtain an estimate of its shape and radius. The sequence of images shown in Figure S1, with increasing magnification, reveal that imaging at very high magnification results in blurriness due to thermal vibration and carbon (or other contaminants) deposition during scanning with the electron beam. In this particular case, the color contrast between Si3N4 and contamination confirms that the tip radius is certainly below 10 nm. To obtain a better estimate of the tip 1 radius, a 1.0 X 1.0 m2 area was scanned on a UNCD surface. The AFM image obtained with this tip (Figure S2a) was later used to predict the tip shape, using the “blind tip estimation” subroutine [1]. A tip radius of 3.6 0.2 nm was calculated, consistent with the SEM metrology (Figure S1) and a tip shape (T) as shown in Figure S2b was predicted. 1 m 50 nm 100 nm Figure S1 SEM images of a commercial Si3N4 probe (from Budgetsensors, Inc.) (a) (b) R = 3.5 nm Figure S2 (a) A 1x1 um2 AFM scan of UNCD substrate obtained with the probe shown in Figure S1; (b) Characterized Tip shape (T) estimated from (a) using the Blind Tip Estimation algorithm [1]. Note that each curve corresponds to a tip cross-section in the xz plane. 2 The tip shape (T) was also used to characterize a larger area (A), 2.5 X 2.5 m2, on the substrate. This characterized area (A) was subsequently scanned before and after wear with other probes to measure its roughness. The estimated tip shape (T) was used to erode the AFM image of area A, to remove the artifact of tip shape (T) from the obtained image. This step yielded the actual surface morphology: Aactual A T , where the ‘-‘ symbol here denotes the erosion operation. Since any arbitrary tip produces images different than Aactual, due to its particular shape, we mathematically perform a dilation operation for parabolic tips of different radius (Tr) to obtain the corresponding surfaces (Ar). In languages of sets, a dilation operation is defined as: Ar Aactual Tr , where the symbol denotes the dilation operation, i.e., adding the artifact of tip Tr to the actual area Aactual The RMS roughness of these mathematically generated surfaces was then calculated and plotted as a function of tip radius. This resulted in a calibration curve (shown in Figure S3) for roughness of the surface measured as a function of the tip radius used to scan the surface. From this calibration curve, the radius of the tip can be estimated based on the roughness of the area (A) measured by the tip. It is important to note that as the tip radius becomes larger, the measured roughness decays abruptly reducing the resolution of the calibration curve. The autocorrelation length () of the surface was measured to be ~180 20nm. From the RMS roughness-tip radius plot, it is apparent that the obtained curve flattens as the tip radius reaches half of the correlation length. Since the larger tip radii can anyways 3 be measured with reasonable accuracy through SEM imaging, the calibration curve reported here is used only when the tip radius was measured to be less than ~90 nm (</2). Figure S3 Calibration curve obtained after dilation of actual UNCD surface to obtain roughness of the surface as a function of the tip radius used to scan the surface. The red line denotes a tip radius equal to half of the surface autocorrelation length. 2. Calculation of Wear Volume Table S1 summarizes the tip radii as measured via SEM imaging and as predicted by the deconvolution method described above. It is noteworthy that the “before wear” measurements of tip radius from both methods are in agreement within ~10% for most of the cases. After wear, the MM remains useful only when the wear is such that the tip maintains its parabolic shape. For example, we found that for an applied contact load of 70 nN, doped and undoped UNCD probes undergo changes too small to be captured by SEM imaging; however the MM showed a change of ~ 2-3 nm. A limitation of the MM is related to the formation of large and sharp asperities during wear as these asperities can 4 produce a very fine AFM image, which might not represent the actual worn tip radius. Likewise, in high wear cases, where the tip shape deviates significantly from being parabolic or the tip diameter becomes comparable to the autocorrelation length (~180 20nm) of the surface (see supporting information), SEM images were used to calculate wear volume. A schematic of the change in profile of an AFM probe before and after wear is shown in Figure S4. Knowing the initial tip radius (Ri), the final tip radius (Rf) after wear, and the tip shape, the volume removed during wear can be calculated using the following formula: V 3 ( R f Ri ) , 3 3 (S1) where is a geometrical factor derived for the conical tip shape and is defined as: cot cos 3 (1 sin ) 2 (2 sin ) , where ( ) is the tip’s half-angle. At high applied contact forces of 200 and 280 nN, the Si3N4 probes were found to be flat after wear and no final radius could be associated with the tips (as shown schematically in Figure S4b). In these cases, the volume lost due to wear was calculated based on a truncated pyramidal geometry with the initial tip radius set to Ri. Note that the geometrical factor and prefactor (/3) are based on the tip shape and instead of being constant they can be a function of tip height; for example, in case of oxide sharpened AFM tips. 5 Table S1 Tip Radius measured before and after wear using two different methodologies. Tip radius using de-convolution method is not reported (represented by a ‘-‘ in the table) wherever tip shape deviated from being parabolic. For doped UNCD, three probes were tested which are reported here. Applied Before Contact or After Force Wear (nN) 70 Before After 100 Before After 130 Before After 175 Before After 200 Before After 280 Before After Silicon Nitride SEM MM (nm) (nm) Doped UNCD SEM MM (nm) (nm) Undoped UNCD SEM MM (nm) (nm) 75 125 42 154 83 ~170 47 ~375 45 Flat 40 Flat 64 65 x x x x 65 204 x x 107 375 32 32 32 88 62 125 38 148 88 175 225 280 68 38 74 42 42 - 61 63 x x x x 63 x x - 24 27 27 46 50 17 80 - Rf Ri Ri (a) 2 (b) 2 6 Figure S4 (a) Schematic of an AFM probe showing the initial and final tip radius and the corresponding volume removed during wear (dark gray). (b) Schematic of an AFM probe with higher contact force such that the tip apex flattens after wear. Dark grey corresponds to removed material. 3. Wear of the substrate The wear of the substrate was found to be negligible, by subsequent measurements with an unworn tip. For example, AFM images in Figure S5 are taken on an area on which wear test was performed with an undoped UNCD probe at 200 nN load. These images were acquired before and after wear experiment, using an unworn tip. Regions 1 and 2 (in dashed lines) show that the topographic features of the substrate are not substantially altered, which confirms that there was no wear of the substrate. Figure S5 AFM images taken with unworn sharp AFM tip before (a) and after (b) wear test. The test in this case was performed with an undoped UNCD probe at applied force of 200 nN. Two regions 1 and 2 are highlighted to show that the substrate wear is negligible as all the features are intact. The 7 offset in the two images is due to the difficulty in finding the exact same area on the substrate after changing AFM tips. 4. Separating the contribution of Fmen and Fadh from pull-off forces Pull-off forces were measured before each wear test and the two contributions were separated. The meniscus force was calculated based on initial tip radius, contact angles and surface tension of water. The difference between pull-off force and meniscus force was attributed to the adhesion force, which was then used to calculate the “work of adhesion”. These results for undoped UNCD probes are given in Table 2 Table 2 Pull-off force measurements before the wear test and the calculation of work of adhesion after subtracting the meniscus forces. Tip Material Case No. 1 2 3 Undoped 4 UNCD 5 6 Initial Tip Radius, Ri (nm) 24 27 50 38 87 225 Pull-off Force, Fpull-off (nN) 18.3 20.9 40.7 32.0 68.0 167.5 Calculated Estimated Meniscus adhesion force, force, Fmen Fadh = Fpull-off (nN) Fmen (nN) 8.9 9.39 10.0 10.81 18.6 22.15 14.1 17.91 32.4 35.67 83.7 83.76 Average value of w Work of adhesion (mJ/m2), w = (Fadh/2Ri) 62.3 63.8 70.5 75.0 65.3 59.3 66.0 ± 5.8 5. Dependence of frictional force on contact area In our study, we verified that the frictional force varies linearly with the contact area. Figure S6 shows the graph of frictional force as a function of contact area for Silicon Nitride and undoped UNCD probes. 8 Friction Force (nN) 2.0 y = 0.3436x + 0.0659 R2 = 0.9386 y = 0.1988x - 0.0335 R2 = 0.9638 1.5 1.0 Silicon Nitride undoped UNCD Linear (Silicon Nitride) Linear (undoped UNCD) 0.5 0.0 3 4 5 6 Contact area (nm2) 7 Figure S6 Plot of frictional force as a function of contact area Reference Villarrubia, J.S., Algorithms for Scanned Probe Microscope Image Simulation, Surface Reconstruction, and Tip Estimation. Journal of Research of the National Institute of Standards and Technology, 1997. 102(4): p. 425. 9