Status of Development of the Future Accelerometers for Next Generation Gravity Missions

The GRACE FO mission, led by the JPL (Jet Propulsion Laboratory) and GFZ (GeoForschungsZentrum), is an Earth-orbiting gravity mission, continuation of the GRACE mission, which will produce an accurate model of the Earth’s gravity field variation providing global climatic data during 5 years at least. Europe and US propose new gravity missions beyond GRACE-FO, with improved performance thanks to laser interferometry and better accelerometers. ONERA has procured the accelerometers for the previous geodetic mission (CHAMP, GRACE, GOCE and now GRACE-FO) and continues to improve the instruments to answer to the challenge of the future missions according to two main domains: Firstly, a new design of electrostatic accelerometer is proposed, based on MicroSTAR configuration, a 3-axes ultra-sensitive accelerometer, with a cubic proof-mass. Secondly, ONERA studies the hybridization of such electrostatic accelerometer with cold atom interferometer technology in order to take advantage of each instrument (high sensitivity for electrostatic accelerometer in short term, and absolute measurement for atom interferometer). A first result of the hybrid instrument, obtained on ground, is presented.

[1]  Hanns Selig,et al.  MICROSCOPE Mission: First Results of a Space Test of the Equivalence Principle. , 2017, Physical review letters.

[2]  Zhongkun Hu,et al.  Demonstration of an ultrahigh-sensitivity atom-interferometry absolute gravimeter , 2013 .

[3]  O. Carraz,et al.  Compact cold atom gravimeter for field applications , 2013, 1302.1518.

[4]  William M. Folkner,et al.  Alternative mission architectures for a gravity recovery satellite mission , 2009 .

[5]  Stefano Cesare,et al.  Next Generation Gravity Mission , 2013 .

[6]  R. Haagmans,et al.  The GOCE gravity mission: ESA's first core explorer , 2007 .

[7]  J. Kusche,et al.  Comparing seven candidate mission configurations for temporal gravity field retrieval through full-scale numerical simulation , 2013, Journal of Geodesy.

[8]  D. Boulanger,et al.  A new generation of ultra-sensitive electrostatic accelerometers for GRACE Follow-on and towards the next generation gravity missions , 2015 .

[9]  A. Landragin,et al.  Stability comparison of two absolute gravimeters: optical versus atomic interferometers , 2014, 1406.5134.

[10]  Frank G. Lemoine,et al.  Design considerations for a dedicated gravity recovery satellite mission consisting of two pairs of satellites , 2012, Journal of Geodesy.

[11]  Hans J. Rath,et al.  The new Drop Tower catapult system , 2005 .

[12]  P. Silvestrin,et al.  Measuring the Earth's gravity field with cold atom interferometers , 2015, 1506.03989.

[13]  Peter Schwintzer,et al.  The CHAMP geopotential mission , 1999 .

[14]  S. Reynaud,et al.  Electrostatic accelerometer with bias rejection for Gravitation and Solar System physics , 2010, 1011.6263.

[15]  A. Landragin,et al.  Detecting inertial effects with airborne matter-wave interferometry , 2011, Nature communications.

[16]  M. Watkins,et al.  The gravity recovery and climate experiment: Mission overview and early results , 2004 .

[17]  Achim Peters,et al.  Mobile quantum gravity sensor with unprecedented stability , 2015, 1512.05660.

[18]  Guillaume Ramillien,et al.  Earth System Mass Transport Mission (e.motion): A Concept for Future Earth Gravity Field Measurements from Space , 2013, Surveys in Geophysics.