Integration time in space experiments to test the equivalence principle

A. M. Nobili, R. Pegna, M. Shao, S. G. Turyshev, G. Catastini, A. Anselmi, R. Spero, S. Doravari, G. L. Comandi, D. M. Lucchesi, and A. De Michele
Phys. Rev. D 89, 042005 – Published 25 February 2014

Abstract

The integration time required by space experiments to perform high accuracy tests of the universality of free fall and the weak equivalence principle is a crucial issue. It is inversely proportional to the square of the acceleration to be measured, which is extremely small; the duration of the mission is a severe limitation and experiments in space lack repeatability. An exceedingly long integration time can therefore rule out a mission target. We have evaluated the integration time due to thermal noise from gas damping, Johnson noise and eddy currents—which are independent of the signal frequency—and to internal damping, which is known to decrease with increasing frequency. It is found that at low frequencies thermal noise from internal damping dominates. In the “Galileo Galilei” proposed space experiment to test the equivalence principle to 1017 the rapid rotation of the satellite (1 Hz) up-converts the signal to a frequency region where thermal noise from internal damping is lower than gas damping and only a factor 2 higher than Johnson noise, with a total integration time of 2.4 to 3.5 hours even in a very conservative estimate. With an adequate readout and additional care in reducing systematics the test could be improved by another order of magnitude, close to 1018, requiring a hundred times longer—still affordable—integration time of 10 to 14.6 days. μSCOPE, a similar room temperature mission under construction by the French space agency to be launched in 2015, aims at a 1015 test with an estimated integration time of 1.4 days. Space tests using cold atoms and atom interferometry have been proposed to be performed on the space station (Q-WEP, to 1014) and on a dedicated mission (STE-QUEST, to 1015 like μSCOPE). In this case integration is required in order to reduce single shot noise. European Space Agency funded studies report an integration time of several months and a few years respectively.

  • Received 1 March 2013

DOI:https://doi.org/10.1103/PhysRevD.89.042005

© 2014 American Physical Society

Authors & Affiliations

A. M. Nobili1,2, R. Pegna2, M. Shao3, S. G. Turyshev3, G. Catastini4, A. Anselmi4, R. Spero3, S. Doravari5, G. L. Comandi2, D. M. Lucchesi2,6, and A. De Michele1

  • 1Department of Physics “E. Fermi,” University of Pisa, Largo B. Pontecorvo 3, 56127 Pisa, Italy
  • 2INFN-Istituto Nazionale di Fisica Nucleare, Sezione di Pisa, Largo B. Pontecorvo 3, 56127 Pisa, Italy
  • 3Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, California 91109, USA
  • 4Thales Alenia Space Italia, Strada Antica di Collegno 253, 10146 Torino, Italy
  • 5California Institute of Technology, Pasadena, California 91109, USA
  • 6INAF-Istituto Nazionale di Astrofisica, IAPS, Via Fosso del Cavaliere 100, 00133 Roma, Italy

  • Corresponding author. nobili@dm.unipi.it

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Issue

Vol. 89, Iss. 4 — 15 February 2014

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