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Applications of Multi-body Dynamical Environments: The ARTEMIS Transfer Trajectory Design (2011)

Woodard, Mark ; Patterson, Chris ; Schlei, Wayne ; [et al.]

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Publication Date: 2019-07-13

Description: 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.

Keywords: Astrodynamics

Type: GSFC-E-DAA-TN15167 , Acta Astronautica (ISSN 0094-5765); 73; 237-249

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