Title of article :
Testing Modified Newtonian Dynamics with LISA Pathfinder Original Research Article
Author/Authors :
Christian Trenkel، نويسنده , , Steve Kemble، نويسنده , , Neil Bevis، نويسنده , , Joao Magueijo، نويسنده ,
Issue Information :
دوهفته نامه با شماره پیاپی سال 2012
Pages :
11
From page :
1570
To page :
1580
Abstract :
We suggest that LISA Pathfinder, a technology demonstrator for the future gravitational wave observatory LISA, could be used to carry out a direct experimental test of Modified Newtonian Dynamics (MOND). The LISA Pathfinder spacecraft is currently being built and the launch date is just a few years away. No modifications of the spacecraft are required, nor any interference with its nominal mission. The basic concept is to fly LISA Pathfinder through the region around the Sun-Earth saddle point, in an extended mission phase, once the original mission goals are achieved. We examine various strategies to reach the saddle point, and find that the preferred strategy, yielding relatively short transfer times of just over 1 year, probably involves a lunar fly-by. LISA Pathfinder will be able to probe the intermediate MOND regime, i.e. the transition between deep MOND and Newtonian gravity. We present robust estimates of the anomalous gravity gradients that LISA Pathfinder should be exposed to, based on MONDian effects as derived from the Tensor-Vector-Scalar (TeVeS) theory. The spacecraft speed and spatial scale of the MOND signal combine in a way that the spectral signature of the signal falls precisely into LISA Pathfinder’s measurement bandwidth. We find that if the gravity gradiometer on-board the spacecraft achieves its currently predicted sensitivity, these anomalous gradients could not just be detected, but measured in some detail.
Keywords :
Experimental gravitation , LISA Pathfinder , Modified Newtonian Dynamics , Fundamental physics in space , Dark matter
Journal title :
Advances in Space Research
Serial Year :
2012
Journal title :
Advances in Space Research
Record number :
1134263
Link To Document :
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