The application of forces in multi-body dynamical environments to permit the transfer of spacecraft from Earth orbit to Sun-Earth weak stability regions and then return to the Earth-Moon libration (L1 and L2) orbits has been successfully accomplished for the first time. This demonstrated that transfer is a positive step in the realization of a design process that can be used to transfer spacecraft with minimal Delta-V expenditures. Initialized using gravity assists to overcome fuel constraints; the ARTEMIS trajectory design has successfully placed two spacecrafts into Earth-Moon libration orbits by means of these applications.
Applications of Multi-body Dynamical Environments: The ARTEMIS Transfer Trajectory Design
Acta Astronautica ; 73
2011-12-23
Sonstige
Keine Angabe
Englisch
Applications of multi-body dynamical environments: The ARTEMIS transfer trajectory design
Online Contents | 2012
|Artemis I Trajectory Design and Optimization
NTIS | 2020
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