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Optimal two-impulse transfers to the libration point $L_2$ of the Sun-Earth system with the use of asymptotic trajectories

A.I. Subaev

Moscow University Physics Bulletin 1991. 46. N 5. P. 105

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It is shown that energy expenditures for a transfer from a near-Earth circular artificial satellite orbit to the libration point $L_2$ of the Sun-Earth system can be reduced, if asymptotic trajectories are used.

Authors

A.I. Subaev
Sternberg State Institute of Astronomy, Moscow State University, Leninskie Gory, Moscow, 119992, Russia

Issue 5, 1991

Moscow University Physics Bulletin

Science News of the Faculty of Physics, Lomonosov Moscow State University

This new information publication, which is intended to convey to the staff, students and graduate students, faculty colleagues and partners of the main achievements of scientists and scientific information on the events in the life of university physicists.