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Thermal Characterization of Emisshield

机译:防辐射罩的热特性

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摘要

Testing was conducted on a high-emissivity nanoparticle ceramic coating (EmisshieldTM) for potential use as anhigh-temperature thermal protection coating on the Rocketplane XP vehicle. Although this product was essentiallyndeveloped for reentry vehicles, it has broad applicability in other high-speed elevated-temperature applications.Thisnwork presents a study of key thermal properties from room temperature up to conditions seen in a mild reentry.nSurface-normal emissivity, thermal conductivity, and heat capacity were evaluated as a function of temperature ton760u0001nC (1400u0001nF). Tests were also performed to determine the thermal-cycling durability and potential for reuse of thenceramic coating applied on metal substrates at elevated temperatures.
机译:测试是在高发射率纳米粒子陶瓷涂层(EmisshieldTM)上进行的,有可能用作Rocketplane XP车辆的高温热保护涂层。尽管该产品本质上是为再入车辆开发的,但它在其他高速高温应用中也具有广泛的适用性。本文研究了从室温到中等再入条件下的关键热性能。n表面正常发射率,导热率并根据温度ton760u0001nC(1400u0001nF)对热容量进行了评估。还进行了测试以确定热循环耐久性和在高温下重涂在金属基材上的陶瓷涂层的再利用潜力。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2009年第1期|p.87-92|共6页
  • 作者单位

    University of Oklahoma, Norman, Oklahoma 73019Rocketplane-Kistler Inc., Oklahoma City, Oklahoma 73159;

  • 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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