摘要
以一种典型的采用高压气体弹射释放技术的载荷分离方案为研究对象,建立了载荷、飞行器分离运动数学模型,通过动力学仿真对载荷的分离运动过程进行了分析,获得了在不同飞行工况条件下的载荷分离运动规律,以及分离过程对飞行器运动的影响,为分离时序、以及分离条件的制定提供了依据.
Aiming at load separation by high pressure gas releasing technology,the mathematical model of the load separating process from a vehicle was built.Dynamic simulation analysis is conducted,the motion law of the load separation under different flight conditions was obtained,and.the influences of separation on the vehicle motion are discussed.The above study can help determine when and on which flight conditions to execute the separation action.
作者
李晓东
渠弘毅
高婷
王蕴宝
张贻进
LI Xiaodong;QU Hongyi;GAO Ting;WANG Yunbao;ZHANG Yijin(Beijing Institute of Space Long March Vehicle,Beijing 100076,China;Military Representative Office of PLA Rocket Force,Beijing 100076,China;Unit 96716 of PLA,Ganzhou 341000,China)
出处
《大连交通大学学报》
CAS
2020年第3期46-50,共5页
Journal of Dalian Jiaotong University
关键词
气体
释放
载荷分离
仿真分析
gas
release
load separation
simulation analysis