EMPIRICAL CONSTRAINTS ON TROJAN COMPANIONS AND ORBITAL ECCENTRICITIES IN 25 TRANSITING EXOPLANETARY SYSTEMS

We present a search for Trojan companions to 25 transiting exoplanets. We use the technique of Ford & Gaudi, in which a difference is sought between the observed transit time and the transit time that is calculated by fitting a two-body Keplerian orbit to the radial-velocity data. This technique...

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Bibliographic Details
Main Authors: Madhusudhan, Nikku (Contributor), Winn, Joshua Nathan (Contributor)
Other Authors: Massachusetts Institute of Technology. Department of Earth, Atmospheric, and Planetary Sciences (Contributor), Massachusetts Institute of Technology. Department of Physics (Contributor), MIT Kavli Institute for Astrophysics and Space Research (Contributor)
Format: Article
Language:English
Published: American Astronomical Society, 2010-02-24T14:25:46Z.
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100 1 0 |a Madhusudhan, Nikku  |e author 
100 1 0 |a Massachusetts Institute of Technology. Department of Earth, Atmospheric, and Planetary Sciences  |e contributor 
100 1 0 |a Massachusetts Institute of Technology. Department of Physics  |e contributor 
100 1 0 |a MIT Kavli Institute for Astrophysics and Space Research  |e contributor 
100 1 0 |a Winn, Joshua Nathan  |e contributor 
100 1 0 |a Madhusudhan, Nikku  |e contributor 
100 1 0 |a Winn, Joshua Nathan  |e contributor 
700 1 0 |a Winn, Joshua Nathan  |e author 
245 0 0 |a EMPIRICAL CONSTRAINTS ON TROJAN COMPANIONS AND ORBITAL ECCENTRICITIES IN 25 TRANSITING EXOPLANETARY SYSTEMS 
260 |b American Astronomical Society,   |c 2010-02-24T14:25:46Z. 
856 |z Get fulltext  |u http://hdl.handle.net/1721.1/51802 
520 |a We present a search for Trojan companions to 25 transiting exoplanets. We use the technique of Ford & Gaudi, in which a difference is sought between the observed transit time and the transit time that is calculated by fitting a two-body Keplerian orbit to the radial-velocity data. This technique is sensitive to the imbalance of mass at the L4/L5 points of the planet-star orbit. No companions were detected above 2σ confidence. The median 2σ upper limit is 56 M ⊕, and the most constraining limit is 2.8 M ⊕ for the case of GJ 436. A similar survey using forthcoming data from the Kepler satellite mission, along with the radial-velocity data that will be needed to confirm transit candidates, will be sensitive to 10-50 M ⊕ Trojan companions in the habitable zones of their parent stars. As a by-product of this study, we present empirical constraints on the eccentricities of the planetary orbits, including those which have previously been assumed to be circular. The limits on eccentricity are of interest for investigations of tidal circularization and for bounding possible systematic errors in the measured planetary radii and the predicted times of secondary eclipses. 
520 |a William S. Edgerly Innovation Fund 
546 |a en_US 
655 7 |a Article 
773 |t Astrophysical Journal