| 航天飞机轨道器着陆阻力伞 |
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| 引用本文： | 赵祖虎.航天飞机轨道器着陆阻力伞[J].航天返回与遥感,1998(3). |
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| 作者姓名： | 赵祖虎 |
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| 作者单位： | 北京空间机电研究所 北京 |
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| 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。
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| 关 键 词： | 航天飞机 降落伞 试验 |
SPACE SHUTTLE ORBITER DRAG PARACHUTE SYSTEM |
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| Zhao Zuhu.SPACE SHUTTLE ORBITER DRAG PARACHUTE SYSTEM[J].Spacecraft Recovery & Remote Sensing,1998(3). |
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| Authors: | Zhao Zuhu |
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| Abstract: | 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. |
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| Keywords: | Space Shuttle Orbiter Parachute Test |
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