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首页> 外文会议>1st International conference on green propellant for space propulsion >EXPERIMENTAL TESTS ON A LAB-SCALE HYBRID ROCKET
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EXPERIMENTAL TESTS ON A LAB-SCALE HYBRID ROCKET

机译：实验室规模混合火箭的实验测试

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摘要

Hybrid propulsion offers many well known advantages. In practice it is not possible to take advantage of these capabilities. In fact, although the hybrid combustion process has been explored for many years, it is still fairly unknown and experimental tests so far have left a number of questions still unresolved. Therefore numerical and experimental studies are in progress at the DISIS in order to achieve fuel configuration and operating conditions suitable to ensure a uniform and complete fuel consumption and a regression rate roughly constant over time. Results of a number of tests with GOX and PE or HTPB as propellants are shown below. In particular, temperature and pressure effects on fuel regression rate measurements by an ultrasounds technique are analyzed and a method to correct temperature effects is proposed.
机译：混合动力提供了许多众所周知的优势。实际上，不可能利用这些功能。实际上，尽管已经对混合燃烧过程进行了多年的探索，但它仍然是一个未知数，到目前为止，实验测试仍未解决许多问题。因此，DISIS正在进行数值和实验研究，以实现适合于确保均匀和完整的燃油消耗以及随着时间推移大致恒定的回归率的燃油配置和运行条件。下面显示了使用GOX和PE或HTPB作为推进剂的许多测试结果。特别地，分析了温度和压力对超声技术对燃料回归率测量的影响，并提出了一种校正温度影响的方法。

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  • 来源
  • 会议地点 Noordwijk(NL)
  • 作者

    A. Russo Sorge; C. Carmicino; L. Ferrazzano; C. Capasso;

  • 作者单位

    Department of Space Science and Engineering "L.G. Napolitano" University of Naples "Federico II", Naples, Italy Tel. +39-081-7682355, Fax +39-081-5932044;

    rnDepartment of Space Science and Engineering "L.G. Napolitano" University of Naples "Federico II", Naples, Italy Tel. +39-081-7682355, Fax +39-081-5932044;

    rnDepartment of Space Science and Engineering "L.G. Napolitano" University of Naples "Federico II", Naples, Italy Tel. +39-081-7682355, Fax +39-081-5932044;

    rnDepartment of Space Science and Engineering "L.G. Napolitano" University of Naples "Federico II", Naples, Italy Tel. +39-081-7682355, Fax +39-081-5932044;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 空气动力学;
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