A Quasi-Stationary Solution to Gliese 436b's Eccentricity

TL;DR

This paper explores how a second planet could maintain Gliese 436b's eccentric orbit through a quasi-stationary state, combining secular theory and numerical simulations to identify potential companion planets.

Contribution

It introduces a secular model incorporating tidal effects to identify stationary configurations of Gliese 436b and a companion, supported by numerical validation.

Findings

Potential companion planets have radial velocity amplitudes around 3 m/s.

Transit timing variations are predicted to be between 1 and 5 seconds.

A specific example suggests a companion with 8.5 Earth masses at 40-day orbit.

Abstract

We investigate the possibility that the large orbital eccentricity of the transiting Neptune-mass planet Gliese 436b is maintained in the face of tidal dissipation by a second planet in the system. We find that the currently observed configuration can be understood if Gliese 436b and a putative companion have evolved to a quasi-stationary fixed point in which the planets' orbital apses are co-linear and in which secular variations in the orbital eccentricities of the two planets have been almost entirely damped out. We adopt an octopole-order secular theory based on a Legendre expansion in the semi-major axis ratio to delineate well-defined regions of (P_c, M_c, e_c) space that can be occupied by a perturbing companion. We incorporate the evolutionary effect of tidal dissipation into our secular model of the system, and solve the resulting initial value problems for a large sample of the allowed configurations. We then polish the stationary configurations derived from secular theory with full numerical integrations. We present our results in the form of candidate companion planets to Gliese 436b. For these candidates, radial velocity half-amplitudes, K_c, are of order 3 m/s, and the maximum amplitude of orbit-to-orbit transit timing variations are of order Delta t=1 s to Delta t=5s. For the particular example case of a perturber with orbital period, P_c=40 d, mass, M_c=8.5 M_Earth, and eccentricity, e_c=0.58, we confirm our semi-analytic calculations with a full numerical 3-body integration of the orbital decay that includes tidal damping and spin evolution. Additionally, we discuss the possibility of many-perturber stationary configurations, utilizing modified Laplace-Lagrange secular theory.