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“火星探测漫游者”降落伞的研制 被引量：1

Development of the Parachute of Mars Exploration Rover
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摘要 概述了“火星探测漫游者”探测器的降落伞系统,并介绍了降落伞系统的组成和性能,以及降落伞的研制过程的主要工作,尤其是设计人员解决和处理的一些细节问题。 This paper summarizes the Mars Exploration Rover （MER）parachute system, intro duces the composition and performance of MER parachute system, and primary work in parachute development, especially includes some detailed problems which have been solved by designers.
作者 陈旭 荣伟 陈国良
机构地区 北京空间机电研究所
出处 《航天器工程》 2007年第2期50-56,共7页 Spacecraft Engineering
关键词 火星着陆 降落伞系统 Mars landing parachute system
分类号 V445 [航空宇航科学与技术—飞行器设计]
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参考文献9

  • 1Edward J,Fallon.System design overview of the Mars Pathfinder parachute decelerator subsystem[]..1997
  • 2Steltzner A,Desai P,Leef W,Brunol R.The Mars Explo-ration Rovers entry descent and landing and the use of aerodynamic decelerators[].th AIAA AerodynamicDecelerator Systems Technology Conference and Semi-nar.2003
  • 3Witkowski A,Bruno R.Mars exploration rover para-chute decelerator system program overview[].th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.2003
  • 4Desai P N,Schofield J T,Lisano ME.Flight reconstruc-tion of the Mars Pathfinder disk-gap-band parachute drag coefficient[].th AIAA Aerodynamic Decelera-tor Systems Technology Conference and Seminar.2003
  • 5Taeger Y,Witkowski A.Asummary of dynamic testing of the Mars Exploration Rover parachute decelerator system[].th AIAA Aerodynamic Decelerator sys-tems Technology Conference and Seminar.2003
  • 6Steltzner A,Cruz J,Bruno R,et al.Opportunities and limitations inlowearth subsonic testing for qualification of extraterrestrial supersonic parachute designs[].th AIAA Aerodynamic Decelerator Systems Technol-ogy Conference and Seminar.2003
  • 7Zell P T,Cruz J R.Structural testing of parachutes inthe national full-scale aerodynamics complex80-by-120-foot Wind tunnel at NASA AMES Research Center[].th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.2003
  • 8Cruz J R,Mineck R E,Keller D F,et al.Wind tunnel tes-ting of various disk-gap-band parachutes[].th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.2003
  • 9Way D W,Desai P N,Engelund WC,et al.Design and a-nalysis of the drop test vehicle for the Mars Exploration Rover parachute structural tests[].th AIAA Aero-dynamic Decelerator Systems Technology Conference and Seminar.2003

同被引文献29

  • 1Niehoff J C. Preliminary payload analysis of automated Mars sample return missions[R].Washington:NASA,1967.
  • 2Spadoni D J,Friedlander A L. Mars surface sample return missions via solar electric propulsion[R].Washington:NASA,1971.
  • 3Satin A L. Mars surface sample return (MSSR) system[R].Washington:NASA,1969.
  • 4Carr M H. Rationale for Mars rover/sample return mission[R].Washington:NASA,1989.
  • 5USRA Advanced Design Team. Mars sample return mission two alternate scenarios[R].Washington:NASA,1991.
  • 6LalkT R,Spence C A. Robotic Mars sample return risk assessment and analysis report[R].Washington:NASA,2003.
  • 7Mars sample return research team. Mars sample return implementation[R].Washington:NASA,2010.
  • 8Pratt L M,Allen C,Allwood A C. Mars Astrobiology Explorer-Cacher:a potential rover mission for 2018[R].Washington:Mid-Range Rover Science Analysis Group,2009.
  • 9Akim E L,Stepanyants V A,Tuchin A G. Motion parameters determination of the SC and Phobos in the project Phobos-Grunt[R].Moscow:Keldysh Institute of Applied Mathematics,2007.
  • 10ESA. European space exploration programme executive summary[R].Paris:ESA,2001.

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航天器工程
2007年 第2期

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