首页>
外国专利>
Method and system for launching satellites on non-coplanar orbits using gravitational assistance from the moon
Method and system for launching satellites on non-coplanar orbits using gravitational assistance from the moon
展开▼
机译:利用月球引力辅助在非共面轨道上发射卫星的方法和系统
展开▼
页面导航
摘要
著录项
相似文献
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.
展开▼