Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
10694402 | Advances in Space Research | 2015 | 10 Pages |
Abstract
This paper is concerned with two-impulse transfers from Earth to Earth-Moon L3 halo orbits. After an orbit injection maneuver from an Earth orbit, a spacecraft travels on a ballistic accelerated manifold trajectory to a position intersection with a halo orbit where an orbit injection maneuver is executed. Although many types of transfers are located, our primary concern is transfers that require either a low transfer time of flight or a small orbit injection maneuver. Several families of transfers lie along the edge of a time of flight/injection maneuver Pareto Front. These families share similar characteristics and are shown to be an extension of a transfer that utilizes a stable invariant manifold. The quickest family of transfers to L3 can be completed in 28.5-33Â days with an injection maneuver of 61.75-130Â m/s, with shorter duration transfers requiring a larger injection maneuver. The family of transfers with the smallest injection maneuvers given a duration limit of 140Â days required 13.45Â m/s.
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Space and Planetary Science
Authors
Kathryn Davis, Jeffrey Parker, Eric Butcher,