典型任务气动辅助变轨节省燃料的条件分析  

Analysis of Fuel-saving Criterion for Typical Aero Assisted Orbit Transfer Mission

作　　者：刘刚[1] 

机构地区：[1]中国运载火箭技术研究院,北京100076

出　　处：《导弹与航天运载技术》2013年第5期4-6,共3页Missiles and Space Vehicles

摘　　要：对HEO-LEO(高地轨道-低地轨道)共面变轨和HEO-LEO异面变轨两个典型任务剖面进行了分析。通过引入理想气动辅助变轨假设,比较了气动辅助变轨和直接变轨所需的速度增量,得出气动辅助变轨节省燃料的条件。The two typical missions of HEO-LEO coplanar orbital transfer and HEO-LEO non-coplanar orbital transfer are analyzed. Based on the hypothesis of ideal aero assisted orbit transfer, the velocity increments needed for aero assisted orbit transfer and direct orbit transfer are compared, and the fuel-saving criterion for aero assisted orbit transfer is obtained.

关 键 词：气动辅助变轨 节省燃料 

分 类 号：TJ760.11[兵器科学与技术—武器系统与运用工程]