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Processing Mechanical Test Specimens of Charred Solid Rocket Motor Insulation Materials

机译:烧焦固体火箭发动机绝缘材料的机械性能试验样品的处理

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摘要

The method described herein for producing test specimens of charred insulation material addresses many of the problems associated with traditional methods. Using a nitrogen-flooded tube furnace with a slow heating rate, premachined pieces of reinforced EPDM insulation were charred and successfully tested to measure the shear strengths of the charred materials. Charred materials from this furnace were virtually identical to material recovered from a fired test motor and tested to prove that each material charred would demonstrate unique properties and morphology.
机译:本文所述的用于制造焦化绝缘材料的试样的方法解决了与传统方法相关的许多问题。使用加热速度慢的充氮管式炉,对预加工的增强EPDM绝缘材料进行了烧焦,并成功进行了测试,以测量烧焦材料的剪切强度。从该熔炉中烧焦的材料实际上与从燃烧的测试电动机中回收的材料相同,并经过测试以证明每种烧焦的材料都将表现出独特的特性和形态。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2009年第6期|1318-1320|共3页
  • 作者单位

    Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061;

    Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061;

  • 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

  • 入库时间 2022-08-18 02:36:38

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