Stage separation of recoverable liquid launch vehicle by using moving pulsating ball analogue for propellant sloshing  

作　　者：Yu LU Baozeng YUE Bailong HAO Bole MA Feng LIU Yuanyuan CHANG 

机构地区：[1]School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China [2]Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China

出　　处：《Chinese Journal of Aeronautics》2024年第2期360-370,共11页中国航空学报（英文版）

基　　金：supported by the National Natural Science Foundation of China(Nos.12132002,12202044)。

摘　　要：In the process of stage separation of recoverable liquid launch vehicles,because of the large amount of residual fuel in the storage tanks,the influence of liquid sloshing on separation safety must be considered.Considering calculation simplicity and operation practicability,the Moving Pulsating Ball Model(MPBM)of large amplitude liquid sloshing is introduced into the calculation of launch vehicle stage separation.Combining the dynamic equation of the model with the energy relationship during"breathing movement",the formula calculating the force of liquid on the rigid body is derived.Compared with the calculations of commercial CFD calculation software,the accuracy of MPBM model is verified.Then,all the external forces and moments are applied to the rigid body of the stages,so that the translational and rotational dynamic equations of the stages are obtained respectively.According to the relative position of the two stages,the geometric shape of the interstage section and the engine of the second stage,the minimum clearance in the separation process can be decided to guarantee that the separation process is safe.

关 键 词：Moving Pulsating Ball Model(MPBM) Dynamics of stage separation Large amplitude sloshing Recoverable liquid launch vehicle Flight dynamics 

分 类 号：V475.1[航空宇航科学与技术—飞行器设计]