关于地球静止卫星远地点变轨策略的札记

Note on Apogee Maneuver Scheme for the Geostationary Satellite

在采用小推力远地点发动机的情况下,地球静止卫星在远地点变轨的策略宜按整星功能实现和优化的原则确定。当推重比大于0.02时,多次变轨比1次变轨节省的推进剂并不明显。

Under the Condition of utilization low-thrust apogee motor, the apogee maneuver scheme for the geostationary satellite is defined by the Principle of realization and optimization of entire satellite function. While thrust-weight-ratio is more than 0.02,it is not obviously that Prope-llant saved by more times maneuver is more than one time maneuver does.