空间飞行器中性浮力实验体结构设计
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Design of the Configuration for Experimental Object of Spacecraft Experiment of Neutral Buoyancy
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    摘要:

    中性浮力地面实验系统的实验体设计问题是有效实现空间飞行器研制阶段地面演示验证实验的关键技术之一。本文根据实验系统的任务需求,对实验体结构系统进行了设计。首先根据阿基米德原理对浮心和重心相对位置进行设计;然后通过对质量特性进行计算,给出了实验体结构的最终设计方案;并进行了物理仿真实验,实验结果证明了设计方案的合理性和可行性。

    Abstract:

    The problem of the experimental object design for ground experiment system of neutral buoyancy was one of the key to achieving demonstration effectually of the development of spacecraft. This paper studied the issues of the configuration design which based on the requirement of the experimental object. First, the relative position of the center of mass and buoyancy was design based on the Archimedean principle. Furthermore, the decision was made for the configuration of the experimental object. At last, the result of the design was verified reasonable by experiment.

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蒋奇英. 空间飞行器中性浮力实验体结构设计[J]. 科学技术与工程, 2011, (12): .
Jiang Qi Ying. Design of the Configuration for Experimental Object of Spacecraft Experiment of Neutral Buoyancy[J]. Science Technology and Engineering,2011,(12).

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  • 收稿日期:2011-02-21
  • 最后修改日期:2011-02-21
  • 录用日期:2011-02-22
  • 在线发布日期: 2011-03-24
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