Investigation of the transfer trajectory to the halo orbit near the L2 libration point in the earth-sun system using the moon's gravity

Astronomy and Astrophysics – Astronomy

Scientific paper

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Cislunar Space, Libration, Orbital Mechanics, Solar Orbits, Spacecraft Orbits, Trajectory Analysis, Earth-Moon System, Lunar Gravitation, Orbital Elements

Scientific paper

The mission scheme for transfer to the halo orbit in the earth-sun system proposed by Farquhar (1991) is studied in connection with the Relikt-2 project. According to this scheme, a spacecraft performs two preliminary revolutions along a high-eccentricity orbit. The orbit parameters are chosen so as to provide a close encounter with the moon at the first half-orbiting during the third revolution. As a result, the spacecraft would enter an orbit asymptotically approaching the halo orbit near L2. The moon's gravity effect allows the spacecraft to reach the halo orbit with much smaller dimensions than in the case of direct transfer. A preliminary analysis of approximate trajectories in 1994 is presented.

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