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Process according to the satellite in not - coplanar orbits with the aid of the moon to be difficult to force
Process according to the satellite in not - coplanar orbits with the aid of the moon to be difficult to force
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机译：在月球的辅助下，卫星在非共面轨道上的处理难以进行。
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摘要
A first satellite is placed practically directly by a launcher in a first final orbit (11, 11bis). br / & a second satellite placed on the same launcher is transferred to a substantially elliptical waiting orbit (12, 12bis), the large axis is oriented so as to intercept the toroidal magnetic circuit formed by the sphere of influence of the moon in its orbit, and then during a maneuver at perigee of the elliptical orbit 12bis (high), one proceeds to the transfer of the second satellite on a lunar transfer orbit (13). br / of change of altitude at perigee, and of inclination of an intermediate orbit (14) on which the second satellite is obtained mainly by gravitational reaction in the sphere of influence of the moon, and during the last operation, the second satellite is placed on a final orbit (15) with the values of the orbital parameters substantially different from those of the orbital parameters of the first final orbit.
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