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Test of the Equivalence Principle in an Einstein ElevatorThe scientific goal of the experiment is to test the equality of gravitational and inertial mass (i.e., to test the Principle of Equivalence) by measuring the independence of the rate of fall of bodies from their compositions. The measurement is accomplished by measuring the relative displacement (or equivalently acceleration) of two falling bodies of different materials which are the proof masses of a differential accelerometer spinning about an horizontal axis to modulate a possible violation signal. A non-zero differential acceleration appearing at the signal frequency will indicate a violation of the Equivalence Principle. The goal of the experiment is to measure the Eotvos ratio og/g (differential acceleration/common acceleration) with a targeted accuracy that is about two orders of magnitude better than the state of the art (presently at several parts in 10(exp 13). The analyses carried out during this first grant year have focused on: (1) evaluation of possible shapes for the proof masses to meet the requirements on the higher-order mass moment disturbances generated by the falling capsule; (2) dynamics of the instrument package and differential acceleration measurement in the presence of errors and imperfections; (3) computation of the inertia characteristic of the instrument package that enable a separation of the signal from the dynamics-related noise; (4) a revised thermal analysis of the instrument package in light of the new conceptual design of the cryostat; (5) the development of a dynamic and control model of the capsule attached to the gondola and balloon to define the requirements for the leveling mechanism (6) a conceptual design of the leveling mechanism that keeps the capsule aligned before release from the balloon; and (7) a new conceptual design of the customized cryostat and a preliminary valuation of its cost. The project also involves an international cooperation with the Institute of Space Physics (IFSI) in Rome, Italy. The group at IFSI is in charge of prototyping the differential accelerometer and carrying out precursor laboratory measurements. During this grant year, our partners analyzed and then designed a new prototype of differential accelerometer that has several characteristics in common with the flight accelerometer at this point of the instrument development. The highlights of these activities are documented in a section of this report.
Document ID
20040058116
Acquisition Source
Headquarters
Document Type
Contractor or Grantee Report
Authors
Shapiro, Irwin I.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Glashow, S.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Lorenzini, E. C.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Cosmo, M. L.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Cheimets, P. N.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Finkelstein, N.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Schneps, M.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2004
Subject Category
Mechanical Engineering
Funding Number(s)
CONTRACT_GRANT: NAG3-2881
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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