Novel spaceways for reaching the Moon: An assessment for exploration

DOI10.1007/s10569-008-9156-3zbMath1154.70339OpenAlexW2011353736WikidataQ123991794 ScholiaQ123991794MaRDI QIDQ1003187

Alessio Di Salvo, Ettore Perozzi

Publication date: 27 February 2009

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-008-9156-3

zbMATH Keywords

ExplorationLunar transfersManifold dynamics

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items

Efficient invariant-manifold, low-thrust planar trajectories to the Moon, Quasi-critical orbits for artificial lunar satellites, Earth-Mars halo to halo low thrust manifold transfers, Low-energy, low-thrust transfers to the Moon, Using space manifold dynamics to deploy a small satellite constellation around the Moon, Indirect transfer to the Earth-Eoon L1 libration point, Application of periapse maps for the design of trajectories near the smaller primary in multi-body regimes, Low-energy transfers to the Moon with long transfer time, Lagrangian coherent structures in the planar elliptic restricted three-body problem

Uses Software

• STK

Cites Work

• Unnamed Item
• Alternative paths to Earth-Moon transfer
• Weak stability boundary trajectories for the deployment of lunar spacecraft constellations
• A note on weak stability boundaries
• Connecting orbits and invariant manifolds in the spatial restricted three-body problem
• Quasi-periodic orbits about the translunar libration point
• On the dynamics of weak stability boundary lunar transfers