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Effect of planetary eccentricity on ballistic capture in the solar system

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Publication:816910
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DOI10.1007/S10569-005-3640-9zbMath1129.70330OpenAlexW1964526102MaRDI QIDQ816910

Paolo Teofilatto, Christian Circi

Publication date: 2 March 2006

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

Full work available at URL: https://doi.org/10.1007/s10569-005-3640-9


zbMATH Keywords

ballistic captureHill's regionselliptic restricted three body probleminterplanetary missionslow energy transfers


Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)


Related Items (6)

Gravitational lunar capture based on bicircular model in restricted four body problem. ⋮ Lunar capture in the planar restricted three-body problem. ⋮ Constructing ballistic capture orbits in the real solar system model. ⋮ Optimal mars transfers for small payload transportation ⋮ Observing Mercury by a quasi-propellantless mission ⋮ Formation of the extreme Kuiper-Belt binary \(2001 \text{QW}_{322}\) through adiabatic switching of orbital elements




Cites Work

  • Low Energy Transit Orbits in the Restricted Three-Body Problems
  • On the dynamics of weak stability boundary lunar transfers




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