月地高速再入返回器与近地轨道返回飞行器相比,气体流动效应更加复杂,对气动数据的精准度要求更为苛刻.因此,气动设计与验证的正确性和全面性是月地高速再入任务成功的关键.本文对月地高速再入气动特点进行了分析,对返回器气动设计方法、气动计算与试验项目、数据综合分析和特种气动问题研究的方法与结果进行了阐述,并给出了飞行结果.飞行结果表明返回器气动设计与验证所获得的各项气动数据满足工程要求. Compared with NEO return vehicles, the gas flow effect is more complicated and the accuracy of pneumatic data is more demanding, so the correctness and comprehensiveness of pneumatic design and verification The key to the success of the mission.In this paper, the aerodynamic characteristics of the high speed reentry of moon are analyzed, the methods and results of the aerodynamic design method, aerodynamic calculation and test project, comprehensive data analysis and special aerodynamic problems of the reflector are described. The results of the flight show that the aerodynamic data obtained from the aerodynamic design and verification of the reflector meet the engineering requirements.