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  • Robert Farquhar, the Father of Halo Orbits and Much More

    Paper number

    IAC-17,E4,1,3,x39878

    Author

    Dr. Irene Farquhar, United States

    Coauthor

    Dr. David Dunham, Kinetx, Inc., United States

    Coauthor

    Mr. Kjell Stakkestad, Kinetx, Inc., United States

    Coauthor

    Mr. James V. McAdams, Johns Hopkins University Applied Physics Laboratory, United States

    Coauthor

    Dr. Bobby Williams, Kinetx, Inc., United States

    Coauthor

    Prof. Roger Maurice Bonnet, COSPAR, France

    Coauthor

    Dr. Florian Renk, European Space Agency (ESA), Germany

    Coauthor

    Prof. Klaus Schilling, Zentrum für Telematik, Germany

    Coauthor

    Prof. Kuninori Uesugi, ISAS/JAXA, Japan

    Coauthor

    Mr. James L. Green, National Aeronautics and Space Administration (NASA)/Goddard Space Flight Center, United States

    Year

    2017

    Abstract
    Robert Farquhar left an impressive trail of accomplishments starting very early in the Space Age. His seminal 1969 Stanford University doctoral thesis, The Control and Use of Libration-Point Satellites, was published in 1970 as NASA Technical Report R-346, still a valuable reference on the topic. He worked with John Breakwell to develop the first theoretical basis of halo orbits about the collinear libration points of the three-body problem. He showed how a satellite in a halo orbit about the Earth-Moon L2 libration point could be used as a communications link for a farside landing. After Apollo, he became interested in multiple comet flyby missions and a halo orbit about the Sun-Earth L1 point. Largely through his efforts, in 1978 ISEE-3 became the first libration-point mission. By taking advantage of ISEE-3’s high-energy orbit relative to the Earth, he used a complex series of lunar swingbys to send ISEE-3 to fly by Comet Giacobini-Zinner in 1985, the first comet mission. A byproduct was his discovery of the double-lunar swingby technique that was not only crucial to ISEE-3’s success, but also used by other international missions that studied the Earth’s geomagnetic environment. Around 1990, Bob was largely responsible for the establishment of NASA’s Discovery program of lower-cost planetary exploration missions. The first-launched of these in 1996 was the Near Earth Asteroid Rendezvous (NEAR) mission to (433) Eros; Bob envisioned its clever orbit and was the Mission Manager following its launch. In 2000, NEAR became the first spacecraft to orbit an asteroid, and the first asteroid lander a year later. Bob was the Mission Manager during the pre-launch and early operations of the MESSENGER mission, which in 2011, became the first spacecraft to orbit Mercury. Bob also was instrumental in establishing the first NASA New Frontiers medium-class planetary mission, called New Horizons, that explored the Pluto system in 2015. Bob played important roles for both the trajectory and the politics to help make the mission a success. Thus, Bob’s legacy extends across the Solar System. Bob lived to relish the successful New Horizons flyby of the Pluto system, but sadly, he passed away 3 months later, before all of the stunning images had been sent back to Earth. Bob’s innovative trajectory designs have been used for many missions, and his ideas are bound to be applied to many future missions.
    Abstract document

    IAC-17,E4,1,3,x39878.brief.pdf

    Manuscript document

    IAC-17,E4,1,3,x39878.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.