1 2 [Geophysical Research Letter] 3 4 [Interseismic deformation of the Shahroud fault system (NE Iran) from Space- 5 borne Radar Interferometry measurements] 6 [Z. Mousavi1, 2, E. Pathier1, R. T. Walker3, A.Walpersdorf1, F. Tavakoli4, H. Nankali4, M. Sedighi4, 7 M-P Doin1] 8 [1) ISTerre, Université Joseph Fourier, CNRS UMR 5275, Grenoble, France (zahra.mousavi@ujf- 9 grenoble.fr) Supporting Information for 10 2) Department of Earth Sciences, Institute for Advanced Studies in Basic Sciences, Zanjan, Iran 11 3) Department of Earth Sciences, University of Oxford, South Parks Road, Oxford, OX1 3AN, UK. 12 4) National Cartographic Center, Geodetic Department, Tehran, Iran] 13 14 15 16 17 18 19 20 Contents of this file 21 Text S1. Removing the tropospheric delay, orbit error and residual DEM 22 The tropospheric delays can be split up into turbulent and stratified components. The 23 effect of the turbulent component on SAR acquisitions can be considered as random in 24 space and time and is mostly topography independent. Therefore it can be reduced by 25 stacking or time-series analysis [Schmidt and Burgmann, 2003]. The vertically stratified 26 component, correlated with topography, is not random in space [Doin et al., 2009] and it 27 should be removed before tectonic interpretation. Here we use the global atmospheric Text S1. Removing the tropospheric delay, orbit error and residual DEM Figures S1 to S5 Tables S1 1 28 model ERA-Interim provided by the European Center for Medium‐Range Weather 29 Forecast (ECMWF) to estimate the tropospheric delay map. ERA‐I is a global 30 atmospheric model on a ∼75 km grid, generated four times per day and on 37 pressure 31 levels. The used global atmospheric model like ERA-I have been shown reducing biases 32 in INSAR multi-years strain rate estimate [Jolivet et al., 2011]. We did a spatial bilinear 33 interpolation for the delay function of ERA data and then a spline interpolation for 34 altitude to predict the delay map for each single image [Jolivet et al., 2011]. Differential 35 delay maps corresponding to each interferogram can be estimated by comparing these 36 delay maps. The residual orbital components due to orbital errors can still be significant, 37 particularly when studying low rates of deformation. Such errors are reduced from the 38 wrapped interferometric phase by searching for a best fitting ramp in range, followed by 39 a best fitting ramp in azimuth. We do not try to correct for more complex orbital error at 40 that stage to avoid removing the tectonic signal. Indeed the interseismic signal related to 41 the SFS that we want to estimate should be mainly localized within a few tens of 42 kilometers from the fault zone as shown on other strike-slip fault studies (e.g. Wright et 43 al. 2001, Wang et al 2009, Jolivet et al 2014). In this case, using a simple phase ramp 44 orbital error model estimated over 300km-long track minimize the risk of removing 45 tectonics signal. Comparison with independent GPS data will be done to check a- 46 posteriori the validity of this assumption. The interferometric phase component due to 47 DEM errors varies with the perpendicular baseline between the two acquisitions and is 48 estimated from wrapped interferograms following the methodology from Ducret et al., 49 [2013]. The main interest of this correction is to reduce the phase variance for helping the 50 unwrapping process. Some residual DEM errors may remain after this step; they are re- 2 51 estimated during the time-series analyses step described hereafter. Then, interferograms 52 are filtered using Goldstein's filter [Goldstein and Werner, 1998] and unwrapped using a 53 branch-cut algorithm [Goldstein et al., 1988]. A careful visual inspection of the corrected 54 interferograms indicates that there is no evidence for any sharp creep deformation signal 55 located along the faults over the 2003 to 2010 period. To investigate the long wavelength 56 tectonic signal due to interseismic strain accumulation, a time series analysis of the 57 selected images has been performed on a pixel basis in order to enhance the signal to 58 noise ratio. 59 Reference: 60 Doin, M. P., C. Lasserre, G. Peltzer, O. Cavalié, and C. Doubre (2009), Corrections of stratified 61 tropospheric delays in SAR interferometry: Validation with global atmospheric models, J. Appl. 62 Geophys., 69, 35–50. 63 Ducret, G., M.-P. Doin, R. Grandin, C. Lasserre, S. Guillaso (2013), DEM Corrections Before Unwrapping 64 in a Small Baseline Strategy for InSAR Time Series Analysis, Geoscience and Remote Sensing 65 Letters, IEEE, Volume: PP , Issue: 99, 1 – 5. 66 67 68 69 70 71 Goldstein, M. R., A. H. Zebker, and C. L. Werner (1988), Satellite radar interferometry: Two-dimensional phase unwrapping, Radio Sci., 23(4), 713–720. Goldstein, M. R., and L. C. Werner (1998), Radar interferogram filtering for geophysical applications, Geophys. Res. Lett., 25(21), 4035–4038. Jolivet, R., R. Grandin, C. Lasserre, M.-P.Doin, and G. Peltzer (2011), Systematic InSAR tropospheric phase delay corrections from globa l meteorological reanalysis data, Geophys. Res. Lett., 38, L17311. 72 Jolivet, R., P. S. Agram, N. Y. Lin, M. Simons, M. P. Doin, G. Peltzer, and Z. Li (2014), Improving InSAR 73 geodesy using global atmospheric models. Journal of Geophysical Research: Solid Earth, 119(3), 74 2324-2341. 3 75 Schmidt, D. A., and R. Bürgmann (2003), Time-dependent land uplift and subsidence in the Santa Clara 76 valley, California, from a large Interferometric synthetic aperture radar data set, J. Geophys. Res., 77 108(B9), 2416 78 79 Wang, H., T. J. Wright, and J. Biggs (2009), Interseismic slip rate of the northwestern Xianshuihe fault from InSAR data, Geophys. Res. Lett. 36, no. 3). 80 Wright, T., B. Parsons, and E. Fielding (2001), Measurement of interseismic strain accumulation across the 81 North Anatolian Fault by satellite radar interferometry, Geophys. Res. Lett. 28, no. 10, 2117-2120. 82 Figures: 83 84 85 86 87 88 89 Figure S1. Diagrams of all processed interferograms selected using a maximum perpendicular baseline criterion (500m). Perpendicular baselines with respect to the July 2003 orbit for descending track D020 (left plot), and January 2004 orbit for ascending track A156 (right plot), are plotted as function of acquisition dates. Track D020 uses 22 images that are combined into 63 interferograms and track A156 uses 23 images that are combined into 51 interferograms. 4 90 91 92 93 Figure S2. Velocity versus altitude for the area covered by track D020 from which it is clear that there is no correlation between altitude and deformation. 94 95 96 97 98 Figure S3. Solution space plot for modeling the location of fault and slip rate for the two tracks A156 (left) and D020 (right). The red stars are the best-solution of modeling the location and slip rate of fault based on fix locking depth at 12km and the green stars are the location of fault that we choose for the 2d modeling of slip rate and locking depth. 5 99 100 101 Figure S4. One example of a perturbed dataset: a) the original interferogram, b) the perturbation image c) perturbed data d) the RMS misfit for perturbed data. 102 6 103 104 105 106 107 Figure S5. Solution space plot for modeling the location of fault and slip rate for the two tracks A156 (left) and D020 (right). The red stars are the best-solution of modeling the location and slip rate of fault based on _x locking depth at 12km and the green stars are the location of fault that we choose for the 2d modeling of slip rate and locking depth. 108 109 Tables: 110 111 112 113 Table S1. Correlation coefficients between LOS mean velocity map and topography, estimated separately on the northern and southern part (with respect to the fault zone) of each InSAR tracks. These values are all low, indicating that there is no significant correlation between the mean velocity and topography. 114 Northern part Southern part 0.1643 0.0733 -0.4874 -0.129 correlation coefficient track D020 correlation coefficient track A156 115 116 7