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LARES, Laser Relativity Satellite LARES,LARES, LaserLaser RelativityRelativity Satellite:Satellite: TowardsTowards aa OneOne PercentPercent MeasurementMeasurement ofof FrameFrame DraggingDragging byby LAGEOS,LAGEOS, LAGEOSLAGEOS 2,2, LARESLARES andand GRACEGRACE by ΙΙΙgnazio Ciufolini presented by Rolf Koenig (Univ. Salento) (GFZ) A. Paolozzi*, E. Pavlis* , R. Koenig* , J. Ries* , R. Matzner* , G. Sindoni*, H. Neumayer* *Sapienza Un. Rome, *Maryland Un ., *GFZ-German Research Centre for Geosciences-Potsdam, *Un. Texas Austin 17 Int. Workshop on Laser Ranging, Bad Kötzting, 16-3-2010 ContentContent BRIEF INTRODUCTION ON FRAME -DRAGGING and GRAVITOMAGNETISM EXPERIMENTS * The 2004 -2007 measurements using the GRACE Earth ’s gravity models and the LAGEOS satellites • * LARES: 2011 DRAGGINGDRAGGING OFOF INERTIALINERTIAL FRAMESFRAMES ((FRAMEFRAME --DRAGGINGDRAGGING asas EinsteinEinstein namednamed itit inin 1913)1913) The “local inertial frames ” are freely falling frames were, locally, we do not “feel ” the gravitational field, examples: an elevator in free fall, a freely orbiting spacecraft. In General Relativity the axes of the local inertial frames are determined by gyroscopes and the gyroscopes are dragged by mass -energy currents, e.g., by the Earth rotation. Thirring 1918 Braginsky, Caves and Thorne 1977 Thorne 1986 I.C. 1994-2001 GRAVITOMAGNETISM:GRAVITOMAGNETISM: ff ramerame --draggingdragging isis alsoalso calledcalled gravitomagnetismgravitomagnetism forfor itsits formalformal analogyanalogy withwith electrodynamicselectrodynamics InIn electrodynamicselectrodynamics aa InIn GeneralGeneral RelativityRelativity aa magneticmagnetic needleneedle isis gyroscopegyroscope isis changingchanging changingchanging itsits itsits orientationorientation (frame(frame -- orientationorientation becausebecause dragging)dragging) becausebecause ofof ofof thethe magneticmagnetic fieldfield thethe gravitomagneticgravitomagnetic andand thethe magneticmagnetic fieldfield andand thethe fieldfield isis generatedgenerated byby gravitomagneticgravitomagnetic fieldfield isis electricelectric currents.currents. generatedgenerated byby massmass currents,currents, suchsuch asas thethe EarthEarth rotationrotation (Earth(Earth angularangular momentum).momentum). GRAVITY PROBE B I.C.-Phys.Rev.Lett., 1986: Use the NODES of two LAGEOS satellites; the orbital plane of these satellites is a huge gyroscope affected by frame-dragging. This is called the Lense-Thirring effect IC, PRL 1986: Use of the nodes of two laser-ranged Satellites to measure the Lense-Thirring effect in order to eliminate the error due to the even zonal harmonics IC IJMPA 1989: Analysis of the orbital perturbations affecting the nodes of LAGEOS-type satellites (1) Use two LAGEOS satellites with supplementary inclinations OR: Use n satellites of LAGEOS-type to measure the first n-1 even zonal harmonics: J 2, J 4, … and the Lense-Thirring effect IC NCA 1996: use the node of LAGEOS and the node of LAGEOS II to measure the Lense-Thirring effect However, in 1996 the two nodes were not enough to measure the Lense-Thirring effect because of the uncertainties in the Earth gravity field 2002 Use of GRACE to test Lense-Thirring at a few percent level: J. Ries et al. 2003 (1999),E. Pavlis 2002 (2000) EIGENEIGEN --GRACE02SGRACE02S ModelModel andand UncertaintiesUncertainties Even Value Uncertainty Uncertainty Uncertainty Uncertainty zonals on node I, on on perigee lm · 10 -6 relative to the Node II, II, relative to frame- relative to the frame- dragging the frame- dragging effect dragging effect effect 202020 0.53 •••101010 −−−10−10 1.59 ΩΩΩ 2.86 Ω 1.17 ω −−− L T L T L T 484.16519788 −−−11−11 4040400.53999294 0.39 •••101010 0.058 ΩΩΩL T 0.02 ΩΩΩL T 0.082 ω L T −−−11−111111 606060−−−.14993038 −.14993038 0.20 •••101010 0.0076 Ω L T 0.012 Ω L T 0.0041 ω L T −−−11−11 8080800.04948789 0.15 •••101010 0.00045 ΩΩΩL T 0.0021 Ω L T 0.0051 ω L T −−−11−11 10,0 0.05332122 0.21 •••101010 0.00042 Ω L T 0.00074 Ω L T 0.0023 ω L T The result was published in Nature Letters in 2004. We measured frame-dragging to be 99 % of its General Relativity prediction with an error of about 10 %. Observed value of Lense-Thirring effect using The combination of the LAGEOS nodes. Observed value of Lense-Thirring effect = 99% of the general relativistic prediction. Fit of linear trend plus 6 known frequencies General relativistic Prediction = 48.2 mas/yr I.C. & E.Pavlis, Letters to NATURE, 431, 958, 2004. NEW 2006-2007 ANALYSIS OF THE LAGEOS ORBITS USING THE GFZ ORBITAL ESTIMATOR EPOS *by adding the geodetic OLD 2004 ANALYSIS OF THE precession of the orbital LAGEOS ORBITS USING THE plane of an Earth satellite NASA ORBITAL ESTIMATOR in the EPOS orbital estimator. GEODYN Comparison of Lense-Thirring effect measured using different Earth gravity field models Each point corresponds to a different GRACE Earth gravity model In 2008 Ries et al. presented independent results for the measurement of frame.draggging by spin using LAGEOS, LAGEOS 2 and the GRACE Earth’s gravity models . John Ries (UT Austin) error budget is of about 12 %. LARESLARES (LAser(LAser RElativityRElativity Satellite)Satellite) ItalianItalian SpaceSpace AgencyAgency WeightWeight aboutabout 400400 kgkg RadiusRadius aboutabout 1818 cmcm MaterialMaterial SolidSolid spheresphere ofof TungstenTungsten alloyalloy SemimajorSemimajor axisaxis aboutabout 79007900 kmkm EccentricityEccentricity nearlynearly zerozero InclinationInclination aboutabout 71.571.5 degreesdegrees CombinedCombined withwith LAGEOSLAGEOS andand LAGEOSLAGEOS 22 datadata itit wouldwould provideprovide aa confirmationconfirmation ofof EinsteinEinstein GeneralGeneral Relativity,Relativity, thethe measurementmeasurement ofof frameframe --draggingdragging withwith accuracyaccuracy ofof aa fewfew percent.percent. LARES design by: Sapienza University of Rome (Antonio Paolozzi and his team) The new VEGA launcher by the European Space Agency, first launch planned at the end of 2011- beginning of 2012, with the LARES payload A BALL OF TUNGSTEN, TO BECAME THE LARES SATELLITE AFTER CARVING THE HOUSING OF THE CCR, COURTESY OF THE ITALIAN SPACE AGENCY LARES DM before mounting the CCR THE LARES SATELLITE AT THE OFFICINE OMPM IN SALERNO Conclusions * Frame-dragging (Lense-Thirring effect) has been measured with accuracy of approximately 10 % using LAGEOS, LAGEOS II and the GRACE Earth’s gravity models. * After a few years of the LARES satellite (to be launched at the end of 2011) laser-ranging data will be available, together with future improved Earth’s gravity models, the accuracy of the frame-dragging measurement should approach 1 %. THE END.
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