月球探测器的软着陆技术  

An Introduction to Soft-landing Techniques for Lunar Lander

作　　者：杨湘杰[1] 刘焕焕[1] 王文林[1] 

机构地区：[1]南昌大学机电工程学院,江西南昌330031

出　　处：《机电产品开发与创新》2008年第3期27-28,33,共3页Development & Innovation of Machinery & Electrical Products

摘　　要：介绍了空间探测中航天器的各种软着陆方式和月球探测器的软着陆特点,对前苏联和美国成功着陆的月球探测器概况进行了综述,并提出了我国在月球探测软着陆器的设计、研制阶段所面临的一些主要课题。A detail introduction was made for various soft landing approaches of space vehicles especially the deceleration and impact energy dissipation techniques for soft lunar landing.The successful lunar landers of the former Union of Soviet Socialist Republics and the United States were briefly summarized.Main research areas for the nowadays Chinese soft lunar lander development project were put forward.

关 键 词：月球探测 有效载荷 软着陆 减速 缓冲 

分 类 号：V47[航空宇航科学与技术—飞行器设计] TH12[机械工程—机械设计及理论]