Transfer trajectory design for the SOHO libration-point mission

Details Transfer trajectory design for the SOHO libration-point mission Transfer trajectory design for the SOHO libration-point mission

Aug 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992wadc.iafct....d&link_type=abstract

IAF, International Astronautical Congress, 43rd, Washington, Aug. 28-Sept. 5, 1992. 12 p.

Astronomy and Astrophysics

Astronomy

Halo Orbit Space Station, Libration, Lissajous Figures, Spacecraft Maneuvers, Transfer Orbits, Interplanetary Trajectories, Solar Wind

Scientific paper

It is shown that transfer trajectories to the halo orbit exist throughout the year, with a one week closure of the launch window each month because of unfavorable lunar perturbations that cannot be corrected in the case of transfer trajectory insertion errors. The launch window for transfers to large-amplitude Lissajous orbits is virtually the same as that for transfers to the baseline halo orbit. Details of these trajectories are described and questions about groundstation coverage are discussed.

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