Physics
Scientist
A Practicable Orbit for a Space Radio Interferometer Station
An Investigation of Trajectories Into a Halo Orbit Near the L/2 Libration Point in the Earth / Sun System by Using the Moon's Gravity
Analytical method for calculation of halo-orbit motion and the problem of screening an artificial satellite from solar radiation in the "Relikt-2" project.
Control characteristics in the insertion of a spacecraft near the L2 point of the Earth-Sun system with the help of lunar gravity (the Relict-2 project).
Earth-Moon-halo orbit flight paths in the vicinity of the Earth-Sun libration point L2.
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