航天飞机轨道器着陆阻力伞  

SPACE SHUTTLE ORBITER DRAG PARACHUTE SYSTEM

作　　者：赵祖虎[1] 

机构地区：[1]北京空间机电研究所,北京100076

出　　处：《航天返回与遥感》1998年第3期11-15,共5页Spacecraft Recovery & Remote Sensing

摘　　要：航天飞机轨道器设置阻力伞的目的在于增加其着陆的安全性。文中不仅介绍了这种阻力伞系统的设计和研制,而且还对试验(风洞试验、B—52飞机着陆试验、飞行模拟和轨道器飞行试验)及为增加阻力伞稳定性和可重复使用性的技术关键作了简要介绍。The desire to increase landing safety margins for the Space Shuttle Orbiter led to decision to implement a Drag Parachute System into the Orbiter Vehicle. This paper not only presents the design and development of this Drag Parachute System, but also briefly discusses wind tunnel tests, B-52 tests, flight simulaters and Orbiter flight testing as well as technical challenges of increasing parachute stability and implementation of reusability.

关 键 词：航天飞机 降落伞 轨道器 阻力伞系统 

分 类 号：V475.2[航空宇航科学与技术—飞行器设计] V445.23