Sun-Earth \(L_1\) and \(L_2\) to Moon transfers exploiting natural dynamics
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Publication:5962792
DOI10.1007/S10569-014-9581-4zbMath1409.70008OpenAlexW1628430719MaRDI QIDQ5962792
Massimiliano Vasile, Willem van der Weg
Publication date: 24 February 2016
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-014-9581-4
survivabilitycoupled circular restricted three-body problemlibration pointlunar capturelunar impactsolar radiation pressureweak capture
Cites Work
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- Solar sail orbits at the Earth-Moon libration points
- A note on weak stability boundaries
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- Dynamics and Mission Design Near Libration Points
- On the Relation Between the Bicircular Model and the Coupled Circular Restricted Three-Body Problem Approximation
- New methods in celestial mechanics and mission design
- Dynamics and Mission Design Near Libration Points
- Low Energy Transit Orbits in the Restricted Three-Body Problems
- Low energy transfer to the Moon
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