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首页> 外文期刊>Journal of Spacecraft and Rockets >Experimental Investigation of Leak-Rate Performance of a Subscale Composite Elastomer-Retainer Docking Seal
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Experimental Investigation of Leak-Rate Performance of a Subscale Composite Elastomer-Retainer Docking Seal

机译:次尺度复合弹性体-固定座对接密封件泄漏率性能的实验研究

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摘要

A novel docking seal was investigated for application to the main interface seal of NASA's low-impact docking system. This interface seal was designed to maintain acceptable leak rates while being exposed to the harsh environmental conditions of outer space. In this experimental evaluation, the leak rate of a candidate docking-seal assembly was characterized and evaluated. The composite seal was manufactured from silicone elastomer S0383-70, vacuum molded into a metal retaining ring. Four seal designs were considered with unique characteristic heights. The leak-rate performance was characterized through a mass point leak-rate method by monitoring gas properties within an internal control volume. The leak rates of the seals were measured at representative docking temperatures of -58, +73, and +122°F for all four seal designs and characterized at 100,74, and 48% of full closure. For all conditions, considered the candidate seal assemblies met the leak-rate criteria derived from the approximate mission requirements.
机译:研究了一种新型对接密封件,该密封件可应用于NASA低冲击对接系统的主界面密封件。该接口密封件设计为在暴露于恶劣的外太空环境条件下时仍可保持可接受的泄漏率。在该实验评估中,对候选对接密封组件的泄漏率进行了表征和评估。复合密封件是由有机硅弹性体S0383-70制造的,真空成型为金属固定环。四个密封设计被认为具有独特的特征高度。通过质量点泄漏率方法通过监测内部控制容积内的气体特性来表征泄漏率性能。对于所有四种密封设计,在代表性的对接温度分别为-58,+ 73和+ 122°F时测量密封的泄漏率,其特征是完全关闭的100,74和48%。在所有情况下,考虑到候选密封组件均符合从近似任务要求得出的泄漏率标准。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2013年第3期|709-714|共6页
  • 作者单位

    College of Engineering,University of Akron, Akron, Ohio 44325-3901;

    College of Engineering,University of Akron, Akron, Ohio 44325-3901;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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