| 摘要 |
<p>The device has two propellant engines (51, 52) that are ready to deliver a push to a geostationary satellite according to axis. The propellant engines are placed on a satellite structure (50) on both sides of a plane containing a center of mass (CM) perpendicular to an axis (Z) of the satellite directed towards the earth. The engines are arranged such that a force resulting from pushes of the engines simultaneously activated pushes a majority component according to another satellite axis (Y) directed perpendicular to the orbit. The engine is a plasma type Hall effect engine. An independent claim is also included for a method for checking slope of orbit for a geostationary satellite.</p> |
