摘要
运载火箭子级的可控回收是运载火箭多次重复使用的基础。提出了一种基于翼伞减速机动、使用飞艇空中捕获的新型运载火箭子级可控回收方案,在运载火箭助推器或一级在分离后的再入过程中采用翼伞系统的大气段减速机动,使用大载重量飞艇群携带捕获网对翼伞飞行器进行空中捕获。开展了总体方案、飞艇捕获方案、飞行控制方案的初步设计和仿真分析,经比较本方案对火箭运载能力和原有设计布局的影响较小,具备后续工程研制和应用的潜力。
In this paper, a novel launch vehicle mid-air recovery technology based on interception with airships is proposed. In this method, parafoil system is applied for aerodynamic deceleration and homing control after stage separation, and the pre-positioned airship group with arresting net would intercept the launch vehicle stage to realize mid-air retrieval. The general scheme including interception system and flight control system are designed, and then, the simulation of process of hitting arresting net is analyzed. Comparing with existing proposals, the influence of launching capability, modification design and scalable capacity are also discussed.
作者
彭越
徐洋
高晨
马小龙
董锴
Peng Yue;Xu Yang;Gao Chen;Ma Xiao-long;Dong Kai(Beijing Institute of Astronautical Systems Engineering,Beijing,100076)
出处
《导弹与航天运载技术》
CSCD
北大核心
2018年第3期27-35,共9页
Missiles and Space Vehicles
关键词
运载火箭
重复使用
可控回收
飞艇捕获
Launch vehicle
Launch vehicle stage recovery
Controllable recovery
Interception with airships
