• DocumentCode
    731568
  • Title

    Testing general relativity during the cruise phase of the BepiColombo mission to Mercury

  • Author

    Imperi, Luigi ; Iess, Luciano

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., Sapienza Univ. of Rome, Rome, Italy
  • fYear
    2015
  • fDate
    4-5 June 2015
  • Firstpage
    135
  • Lastpage
    140
  • Abstract
    General relativity (GR) predicts that photons are delayed and deflected by the space curvature produced by any mass. The Post-Newtonian (PN) parameter controlling the curvature induced by a gravitational field is γ, with bending and delay effects proportional to (γ + 1). γ = 1 in GR. The most accurate estimation of this PN parameter γ = (1 + (2.1 ± 2.3)) · 10-5, has been obtained by the NASA mission Cassini [1] exploiting the frequency shift of radio signal during a Superior Solar Conjunction (SSC) in 2002, while the spacecraft was in cruise to Saturn. The crucial element of the experiment was an advanced radio system providing a highly stable multi-frequency radio link in X and Ka band (8.4 and 32.5 GHz), and a nearly complete cancellation of the plasma noise introduced by the solar corona in Doppler measurements. The ESA-JAXA mission BepiColombo to Mercury will improve the Cassini radio instrumentation by enabling the ranging function also in the Ka band radio link used by the Mercury Orbiter Radio science Experiment (MORE). The fully digital architecture of the transponder provides a pseudo-noie modulation of the carrier at 24 Mcps and a two-way range accuracy of 20 cm. Thanks to the simultaneous tracking by means of the standard telecommunication link, both range and range rate observables will be available for new, more accurate tests of GR. This paper reports on the simulations carried out in order to assess the attainable accuracies in the estimation of γ during the cruise phase of BepiColombo. In an optimal configuration, an uncertainty of 5·10-6 may be attained.
  • Keywords
    Mercury (planet); general relativity; photons; BepiColombo mission phase; Cassini; Cassini radio instrumentation; Doppler measurement; ESA-JAXA mission; GR bending effect; GR delay effect; Ka band highly stable multi-frequency radio link; Ka band radio ranging function; MORE; Mercury; Mercury Orbiter Radio science Experiment; NASA mission; PN parameter; PN parameter control; Post-Newtonian parameter control; SSC; Saturn; X band highly stable multi-frequency radio link; deflected photon prediction; delayed photon prediction; gamma estimation accuracy; general relativity; gravitational field; plasma noise complete cancellation; pseudo-noie modulation; radio signal frequency shift; solar corona; space curvature; standard telecommunication link; superior solar conjunction; transponder fully digital architecture; Accuracy; Extraterrestrial measurements; Gravity; Noise; Planets; Plasmas; Space vehicles; Bepi-Colombo; General Relativity; Mercury; Radio Science; Superior Conjunction;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Metrology for Aerospace (MetroAeroSpace), 2015 IEEE
  • Conference_Location
    Benevento
  • Type

    conf

  • DOI
    10.1109/MetroAeroSpace.2015.7180641
  • Filename
    7180641