%0 Thesis
%A Boudad, Kenza K.
%D 2019
%T Disposal Dynamics from the Vicinity of Near Rectilinear Halo Orbits in the Earth-Moon-Sun System
%U https://hammer.purdue.edu/articles/thesis/Disposal_Dynamics_from_the_Vicinity_of_Near_Rectilinear_Halo_Orbits_in_the_Earth-Moon-Sun_System/7413359
%R 10.25394/PGS.7413359.v1
%2 https://hammer.purdue.edu/ndownloader/files/13716821
%K disposal
%K orbital
%K mechanics
%K CR3BP
%K BCR4BP
%K NRHO
%K bicircular
%K three-body
%K four-body
%K Aerospace Engineering
%X
After completion of a resupply mission to NASA’s proposed Lunar Orbital Platform - Gateway, safe disposal of the Logistics Module is required. One potential option is disposal to heliocentric space. This investigation includes an exploration of the trajectory escape dynamics from an Earth-Moon L2 Near Rectilinear Halo Orbit (NRHO). The effects of the solar gravitational perturbations are assessed in the Bicircular Restricted 4-Body Problem (BCR4BP), as defined in the Earth-Moon rotating frame and in the Sun-B1 rotating frame, where B1 is the Earth-Moon barycenter. Disposal trajectories candidates are classified in three outcomes: direct escape, in direct escapes and captures.
Characteristics of each outcome is defined in terms of three parameters: the location of the apoapses within to the Sun-B1 rotating frame, a characteristic Hamiltonian value, and the osculating eccentricity with respect to the Earth-Moon barycenter. Sample trajectories are presented for each outcome. Low-cost disposal options are introduced.
%I Purdue University Graduate School