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阿里安5助推器回收系统 被引量:3

ARIANE - 5 BOOSTER RECOVERY SYSTEM
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摘要 阿里安5是西欧正在研制的一种大型运载火箭。高度可靠和价廉是它的设计宗旨。发射以后,对助推器进行回收、修复并重复使用,是实现价廉目标的重要手段。文中对这种回收系统的技术要求、主要分系统及回收程序等作了简要介绍。 The Ariane-5 heavy-lift vehicle designed for high reliability and minimum cost is presently under development in Europe. The boosters recovery and reuse after flight is therefore considered to be of great interest for meeting minimum cost. In this paper, the technical requirements and the main subassembly and the recovery sequence of the booster recovery system are briefly introduced.
作者 赵祖虎
出处 《航天返回与遥感》 1996年第4期1-7,共7页 Spacecraft Recovery & Remote Sensing
关键词 运载火箭 助推器 回收 降落伞 Launch vehicle Booster Recovery Parachute
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同被引文献28

  • 1张有济.战术导弹飞行力学设计[M].北京:中国宇航出版社,1996.
  • 2King R, Hengel J E, Wolf D. Ares I first stage booster deceleration system: an overview[C]. Washington: 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, AIAA-2009-2984, 2009.
  • 3Meiboom F P. Aerodynamic characterisation and trajectory simulations for the Ariane-5 booster recovery system[R]. AIAA-93-1214, 1993.
  • 4Purinton D C, Blevins J A, Pritchett V. Aerodynamic characterization and simulation of a solid rocket booster during reentry flight[C]. Orland: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, A1AA-2011-14, 2011.
  • 5Tong D. Payload vehicle aerodynamic reentry analysis[R]. AIAA-91- 0865-CP, 1991.
  • 6Jorgensen L H. Prediction of static aerodynamic characteristics for space-shuttle-like and other bodies at angles of attack from 0° to 180° [R]. NASA, TN D-6996, 1973.
  • 7Hopkins E J. Charts for turbulent skin friction from the van driest method(11)[R]. NASA, TN D-6945, 1972.
  • 8Moore D R, Phelps J, Wood T D. The reusable solid rocket booster (RSRB) a booster system[C]. LongBeach, California: A1AA SPACE 2011 Conference & Exposition, AIAA-2011-7156, 2011.
  • 9Karmer H S, Hengel J. Solid rocket booster compartment pressure flight data analysis[R]. AIAA-2001-2995, 2001.
  • 10赵祖虎.航天飞机助推器轻型回收系统[J].航天返回与遥感,1997,18(4):3-8. 被引量:7

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