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Unsteady flow inferred for Thwaites Glacier, and comparison with Pine Island Glacier, West Antarctica

Published online by Cambridge University Press:  08 September 2017

Jonathan Bamber
Affiliation:
Centre for Polar Observations and Modelling, Bristol Glaciology Centre, University of Bristol, University Road, Bristol BS81SS, England E-mail: j.lbamber@bristol.ac.uk
Eric Rignot
Affiliation:
Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, California 91109-8099, U.S.A.
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Abstract

We present a comparison of surface velocities in 1996, derived from interferometric synthetic aperture radar, with an estimate of the long-term, depth-averaged velocity based on the assumption of steady-state flow for both Pine Island Glacier and its neighbour, Thwaites Glacier, West Antarctica. The results show that the former was close to balance conditions in 1996 (within 9%). The ice flux and velocity of the latter is significantly different in magnitude and distribution from that required to maintain the basin in a state of mass balance over the long term. The balance flux was found to be 32 ± 19% less than the measured outgoing flux. We conclude that the mass imbalance and dramatic difference in the pattern of flow is most likely due to a substantial change in the flow regime of Thwaites Glacier in the recent past.

Information

Type
Research Article
Copyright
Copyright © International Glaciological Society 2002
Figure 0

Fig. 1. Map of the area, showing the locations of in situ accumulation measurements, the glacier locations, and their catchment areas derived from a digital elevation model (DEM) of the ice sheet (Vaughan and others, 2001). The coverage of airborne radio-echo sounding (RES) measurements is shown by grey lines, and spot estimates of ice thickness by circles. The larger solid circles indicate the location of accumulation measurements. Also shown are the areas used as velocity control for the interferometry.

Figure 1

Fig 2. (a) Surface slopes of 0–1° derived from a 5 km spacing DEM of the ice sheet (Bamber and Bindschadler, 1997). (b) Shaded relief plot of surface elevation covering PIG and TWG. The locations of the elevation profiles plotted in Figure 3 are indicated by the thick solid lines.

Figure 2

Fig. 3. (a) Comparison of elevations on PIG. The solid line is from airborne RES measurements, and the dashed line shows elevations interpolated from the DEM. (b) As for (a) but for TWG. The locations of both profiles are shown in Figures 2b, 4 and 5.

Figure 3

Fig. 4. Plots of (a) InSAR velocity (Uinsar) and (b) balance velocity (Ub) for PIG. The direction and magnitude of flow is indicated by the black arrows, with the maximum length equating to a velocity of 1000 m a−1 The grounding line, as determined by interferometry and used to estimate fluxes, is shown as a solid blue line. The locations of ice-thickness flight-lines are shown by the green lines. The dashed sections indicate the locations of the elevation profiles plotted in Figure 3. Ice thickness was also determined close to the grounding line, based on the assumption of hydrostatic equilibrium and a knowledge of the surface elevation and densities of sea water and ice. The black areas within the area of coverage of the SAR data are where it was not possible to obtain interferometrically derived velocity.

Figure 4

Fig. 5. (a, b) As for Figure 4, but for TWG. The maximum length of the arrows is equivalent to a velocity of 2000 m a−1

Figure 5

Fig. 6. The difference in velocity, ΔU(Ub − Uinsar), for the grounded part of TWG, ranging from −500 to 500 m a−1. The RES flight-line, along which Ub and Uinsar are compared in Figure 8, is shown by the solid yellow line. Areas shaded white are where there were no valid velocity data for Ub and/or Uinsar.

Figure 6

Fig. 7. InSAR (points) and balance velocities (solid line) for the grounding lines of (a) PIG and (b) TWG. The lines run north–south and east–west, respectively, (c) Ice thickness along the grounding line derived from the BEDMAP dataset (solid line). The two crosses indicate the position of measured thicknesses. The dots indicate the thickness that would be required to make the balance velocities match the InSAR values.

Figure 7

Fig. 8. A graph of balance velocity (solid line) and InSAR-derived velocity (crosses) along the flight-line shown in Figure 6 for TWG. Also plotted is the measured ice thickness (dashed line). The track is plotted south–north, and the change in direction at about 75.5° S, 105° W takes place about 110 km along-track.