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Force-perturbation analysis of Pine Island Glacier, Antarctica, suggests cause for recent acceleration

Published online by Cambridge University Press:  14 September 2017

Robert Thomas
Affiliation:
EG&G Services, NASA Wallops Flight Facility, Building N-159, Wallops Island, VA 23337, USA E-mail: thomas@osb.wff.nasa.gov
Eric Rignot
Affiliation:
Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099, USA
Pannirselvam Kanagaratnam
Affiliation:
Radar Systems and Remote Sensing Laboratory, University of Kansas, 2335 Irving Hill Road, Lawrence KS 66045-7612, USA
William Krabill
Affiliation:
Code 972, NASA Wallops Flight Facility, Building N-159, Wallops Island VA 23337, USA
Gino Casassa
Affiliation:
Centro de Estudios Cientificos, Av. Arturo Prat 514, Valdivia, Casilla 1469, Chile
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Abstract

Pine Island Glacier, flowing into the Amundsen Sea from West Antarctica, thinned substantially during the 1990s, its grounding line receded by several km, and its velocity increased by >10% to values approaching 3 km a–1. Here, we use these observations, together with estimates of ice thickness and surface strain rates, to estimate the perturbation in forces resisting ice flow compatible with the observations. The analysis assumes that such perturbations are transmitted far upstream from where they originate, and that creep response to the perturbations can be described by equations similar to those that govern ice-shelf creep. It indicates that observed acceleration between 1996 and 2000 could have been caused by progressive ungrounding within the most seaward 25 km ‘ice plain’ of the grounded glacier. Earlier retreat and thinning of the glacier’s floating ice shelf may have provided the conditions that initiated ungrounding of the ice plain. Our analysis indicates that continued ice-plain thinning at the current rate of about 2 ma–1 will result in a velocity increase by 1 km a–1 within the next 11 years as the ice plain becomes totally ungrounded.

Information

Type
Research Article
Copyright
Copyright © The Author(s) [year] 2004
Figure 0

Fig. 1. Pine Island Glacier, showing the CECS/NASA flight track (white line) approximately along the glacier center line, as defined by the velocity maxima. Colors depict velocities inferred from InSAR analysis of ERS data. The 1996 grounding line is shown by the solid line approximately 60 km from the western end of the flight track.

Figure 1

Fig. 2. (a) PIG surface and bed profiles. (b) Velocities and thinning rates along the glacier: upper line is velocity in 2000; middle line is velocity in 1996; bottom line is average thinning rate, 1992–99. (c) Calculated marginal (upper line), driving (middle line) and basal (lower line) shear stresses.

Figure 2

Fig. 3. Longitudinal strain rates derived from observed 1996 velocities, and corresponding lateral strain rates calculated as described in the text.

Figure 3

Fig. 4. Force reduction/unit width (ΔF) on PIG, consistent with velocity increases and thickness changes between 1996 and 2000, plotted against distance from the grounding line. Uncertainty limits are large, so the variation of ΔF is probably adequately represented by the bold line.

Figure 4

Fig. 5. Profiles near the grounding line of PIG, based on measurements in December 2002. The upper line is the surface elevation; the middle line is the ‘hydrostatic elevation’, at which the glacier would become afloat; and the lower line is the difference between these two elevations, which is the thinning required to float the ice. Over the 25 km nearest the grounding line, the maximum surface elevation above hydrostatic elevation is <40 m, with an average value of 20 m. This region is referred to as an ‘ice plain’, and within it there are sections that are either floating or very close to flotation. Continued thinning will enlarge these sections, and the most seaward 10 km of the ice plain appears to be particularly vulnerable, indicating a probable 10 km grounding-line retreat very soon, followed by delayed flotation of the remaining ice plain. Such intermittent ungrounding could explain the sporadic velocity increases reviewed by Joughin and others (2003).

Figure 5

Fig. 6. PIG ice velocities. Curve a was derived from 1996 data; b shows calculated velocities for instantaneous flotation of the ice plain; c shows velocities after progressive ungrounding of the ice plain over about 8 years, neglecting negative feedback from increasing marginal shear stresses; and d shows velocities after progressive ungrounding over 11 years, taking account of this feedback.