This paper presents a proof of concept an feasibility assessment of such a system, demonstrating 38% cost savings for a baseline mission.
Low Earth orbit constellation design using the Earth-Moon L1 point
01.02.2004
Preprint
Keine Angabe
Englisch
Low Earth Orbit Constellation Design Using the Earth-Moon L1 Point (AAS 04-248)
British Library Conference Proceedings | 2005
|Moon global positioning constellation design method based on earth-moon space DRO reference orbit
Europäisches Patentamt | 2024
|Design method of earth-moon system L1 point translation point orbit-earth low-energy transfer orbit
Europäisches Patentamt | 2024
|Sun-Earth Harmonic Orbit via Earth-Moon Resonance Orbit
AIAA | 2024
|Midway correction method for earth-moon L2 point transfer orbit
Europäisches Patentamt | 2020
|