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月球着陆器着陆缓冲机构设计方法研究
引用本文:曾福明,杨建中,满剑锋,朱汪,徐青华,罗敏.月球着陆器着陆缓冲机构设计方法研究[J].航天器工程,2011(2):46-51.
作者姓名:曾福明  杨建中  满剑锋  朱汪  徐青华  罗敏
作者单位:北京空间飞行器总体设计部,北京,100094
摘    要:着陆缓冲机构是着陆器实现月球或行星探测软着陆的关键部件之一,它直接关系到软着陆探测任务的成败.文章根据着陆缓冲机构的功能和特点,提出了从概念设计、方案比较到方案确定、详细分析和试验验证的方案设计流程,并结合月球着陆器着陆缓冲机构的研制经验,对每个阶段的设计方法进行了阐述,可供后续深空探测任务着陆缓冲机构设计借鉴和参考.

关 键 词:月球着陆器  着陆缓冲机构  方案设计  性能分析  方法研究

Study on Design Method of Landing Gear for Lunar Lander
ZENG Fuming,YANG Jianzhong,MAN Jianfeng,ZHU Wang,XU Qinghua,LUO Min.Study on Design Method of Landing Gear for Lunar Lander[J].Spacecraft Engineering,2011(2):46-51.
Authors:ZENG Fuming  YANG Jianzhong  MAN Jianfeng  ZHU Wang  XU Qinghua  LUO Min
Institution:(Beijing Institute of Spacecraft System Engineering, Beijing 100094,China)
Abstract:Landing gear is a key component for soft-landing exploration on the Moon or planet, which determines directly the success of soft-landing exploration mission. Based on the functions and characteristics of landing devices, this paper presents a design guideline which consists of concept design, scheme comparison, scheme confirmation, detailed analysis, and test verification. The design method of each step is also shown, which combines the research experience from soft-landing gear designs of lunar lander. The landing gear design method and process can be used as a reference to soft-landing and buffer gear design in the subsequent deep space exploration mis- sions.
Keywords:lunar lander  landing gear  schematic design  performance analysis  method study
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