NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of various two synodic period Earth-Mars cycler trajectoriesTrajectories that regularly encounter Earth and Mars but use small or no propulsive maneuvers are known as cycler trajectories, or cyclers. For cyclers that repeat after two Earth-Mars synodic periods, several variations are possible. A detailed investigation is presented of a simple two synodic period cycler, along with several promising variations using combinations of one year and half-year phasing orbits. Analysis is included for both the circular co-planar model and with actual Earth and Mars ephemerides.
Document ID
20060029853
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Byrnes, D. V.
McConaghy, T. T.
Longuski, J. M.
Date Acquired
August 23, 2013
Publication Date
August 4, 2002
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Other
Keywords
trajectory cycler repeat orbits

Available Downloads

There are no available downloads for this record.
No Preview Available