In the case of finite thrust apogee maneuver for the geostationary satellite,the fuel consumption increases due to the long burn arc.
推力有限时,地球同步轨道卫星在远地点变轨的弧段很长,会导致较多的燃料消耗。
本网站所收集内容来自网友分享仅供参考,实际请以各学校实际公布信息为主!内容侵权及错误投诉:1553292129@qq.com
CopyRight © 2020-2024 优校网[www.youxiaow.com]版权所有 All Rights Reserved. ICP备案号:浙ICP备2024058711号