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火星探测器降落伞系统综述 被引量：10

Mars Explorer's Parachute System Overview
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摘要 文章介绍了美国火星探测器降落伞系统组成和验证试验情况;分析了5种不同探测器降落伞系统的具体差异;归纳了探测器降落伞系统的结构和性能参数;重点介绍了"凤凰号"和"火星科学实验室"降落伞系统研制过程和性能验证试验。 Mars Explorer＇s Parachute System and its test were particularly presented. And the particular difference in five Parachute Systems was analyzed. Parachute system＇ s structure and performance parameter were concluded. EspeciaUy, parachute system＇s development process and performance test in PHX and MSL were provided.
作者 于莹潇 田佳林
机构地区 空军航空大学航空救生系
出处 《航天返回与遥感》 2007年第4期12-16,共5页 Spacecraft Recovery & Remote Sensing
关键词 落伞系统 盘-缝-带伞 射伞筒 火星探测器 Parachute system Disk- gap- band parachute Mortar Mars explorer
分类号 V445.23 [航空宇航科学与技术—飞行器设计]
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参考文献5

  • 1荣伟,陈旭.火星探测用降落伞研制试验简介[J].航天返回与遥感,2007,28(1):12-17. 被引量：12
  • 2David W W,et al. Mars Science Laboratory: Entry, Descent, and Landing System Performance[ C ], Aerospace Conference, 2007 IEEE.
  • 3Allen Witkowski, et al. Mars 2007 Scout Phoenix Parachute Decelerator System Program Overview [C]. Aerospace Coderence, 2007 IEEE.
  • 4Pamela Hoffman,et al. Preliminary Design of the Cruise, Entry, Descent, and Landing Mechanical Subsystem for MSL [ C]. Aerospace Conference, 2007 IEEE.
  • 5Anita Sengupta, et al. An Overview of the Mars Science ratory Parachute Decelerator System [C]. Aerospace Conference, 2007 IEEE.

二级参考文献20

  • 1Prasun N.Desai.et al.Flight Reconstruction of Mars Pathfinder Disk-Gap-Band Parachute Drag Coefficient,Desai[R].AIAA2003-2126,2003
  • 2Peter T.Zell.et al.Structural Testing of Parachute in the National Full-Scale Aerodynamics Complex 80 by 120 foot Wind Tunnel at NASA Ames[R].AIAA2003-2130,2003
  • 3Edward J.Fallon.System Design Overview of the Mars Pathfinder Parachute Decelerator Subsystem[R].AIAA-97-1511,1997
  • 4Allen Witkowski.et al.Mars Exploration Rover Parachute Decelerator System Program Overview[R].AIAA2003-2100,2003
  • 5Richard A.Lau.et al.The Viking Mars Lander Decelerator System[R].AIAA 70-1162,1970
  • 6Harold N.Murrow.et al.Low-and High-Altitude Tests of Parachutes Designed for Use in Low-Density Atmospheres[R].AIAA 70-1164,1970
  • 7Harold N.Murrow.et al.Some Test Result from the NASA Planetary Entry Parachute Program[J].Spacecraft.1969,16(5)
  • 8Charles H.Whitlock.et al.Inflation and Performance of Three Parachute Configurations from Supersonic Flight Tests in a Low-Density Environment[R].NASA TN D-5296,1969
  • 9James L.Raper.et al.The Viking Parachute Qualification Test Technique[R].AIAA Paper No.73-456,1973
  • 10Clinton V.Eckstrom.et al.Flight Test of a 40-Foot-Nominal-Diameter Disk-Gap-Band Parachute Deployed at a Mach Number of 2.72 and a Dynamic Pressure of 9.7 Pounds for Square Foot[R].NASA TM X-1623,1968

共引文献11

同被引文献53

引证文献10

二级引证文献36

航天返回与遥感
2007年 第4期

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