Abstract
This paper is concerned with two-impulse transfers from Earth to Earth-Moon L 3 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 L 3 can be completed in 28.5-33 days with an injection maneuver of 61.75-130 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 140 days required 13.45 m/s.
Original language | English (US) |
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Pages (from-to) | 1868-1877 |
Number of pages | 10 |
Journal | Advances in Space Research |
Volume | 55 |
Issue number | 7 |
DOIs | |
State | Published - 2015 |
Keywords
- Dynamical systems theory
- Invariant manifolds
- Libration point orbits
- Orbit transfers
- Three-Body trajectories
ASJC Scopus subject areas
- Aerospace Engineering
- Astronomy and Astrophysics
- Geophysics
- Atmospheric Science
- Space and Planetary Science
- General Earth and Planetary Sciences