期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

空间展开机构初步原理分析与方案构想

Elementary Scheme Conception and Principle Analysis of Space Deployable Structure
下载PDF
导出
摘要 文章论述了空间精密展开机构的特点及设计原理,并对展开机构的支撑形式以及关键部件进行了分析及提出构想。 The paper describes the features and design principles of space fine deployable structure, combines with the requirements of the project analyses the support structure and key components, provides the elementary scheme conception of the structure.
作者 王永辉 陈晓丽 李博 刘义良 李玉高 杨秉新
机构地区 北京空间机电研究所
出处 《航天返回与遥感》 2006年第4期38-43,共6页 Spacecraft Recovery & Remote Sensing
关键词 展开机构 铰链 锁定机构 Deployable mechanism Hinge latch
分类号 V414 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献11

  • 1Mark S. Lake etc. A Deployable Primary Mirror for Space Telescopes. SPIE,2.002, 3785:14 - 25.
  • 2S. J. Bullock, L.D. Peterson. Identification of Nonlinear Micron- Level Mechanics for A Precision Deployable Joint. AIAA - 94- 1347- CP, Structual Dynamics, and Matorials Conference,35th, Washington, DC, 1994
  • 3Peter A.Warren. Lightweight, Precision, Deployable Structures. SPIE, 2002,3785:55 - 61
  • 4Mark S. Lake etc. Experimental Characterization of Hysteresis inA Revolute Joint for Precision Deployable Structures. AIAA -2000- 1409 Structures, Structural Dynamics, and Material Conference and Exhibit, 38th, Kissimmee, FL, 1997.
  • 5Alain Carrier etc. Development and Demonstration of A Precision Latch for Deployable Optical Systems.SPIE, 2003, 4850:286-303
  • 6Jeanette L. Domber etc. The Deployment Repeatability of A High Stiffness Folded Composite Hinge. AIAA - 2001 - 1539
  • 7Alain Carrier etc. Development and Microdynamics Characterization of A Deployable Petal Assembly at Full Scale. SPIE,2003, 4850: 254 - 273 Structures, Structural Dynamics, and Materials Conference and Exhibit, 42nd, seattle, WA,2001
  • 8Mark S. Lake, M. Roman Hachkowski. Mechanism Design Principle for Optical - Precision, Deployable Instruments. AIAA -2000- 1409 Structures, Structural Dynamics, and Material Conference and Exhibit, 41st, Atlanta, GA, 2000
  • 9Mark S.Lake, M.Roman Hachkowski.Mechanism Design of Mechanisms for Deployable, Optical Instruments: Guidelines for Reducing Hysteresis. NASA/TM- 2000 - 210089 http://snowwhite: colorado. edu/library/Public Domain/lalce/Design- Guide - 1. pdf
  • 10James E. Phelps. Fabrication and Assembly of High - Preci-sion Hinge and Latch Joints for Deployable Optical Instruments NASA/CR- 1999- 209117 1999 ntrs nasa gov/archive/nasa/casi. ntrs. nasa. gov/19990063541-1999100214. pdf
航天返回与遥感
2006年 第4期

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部