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国外RBCC发动机技术专利分析 被引量:3

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摘要 针对火箭基组合循环发动机的发展现状,通过检索分析国外相关文献和专利,分析了美国、俄罗斯、欧洲等国家和地区火箭基组合循环发动机研究现状,研究了专利申请高潮与技术研发计划的关系,分析了总体设计方案、进气道技术、燃烧系统等关键技术的最新研究进展。
出处 《飞航导弹》 北大核心 2015年第4期78-82,共5页 AERODYNAMIC MISSILE JOURNAL
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参考文献13

  • 1张鹏峰.国外RBCC组合循环发动机发展趋势及关键技术[J].飞航导弹,2013(8):68-71. 被引量:10
  • 2秦飞,吕翔,刘佩进,何国强.火箭基组合推进研究现状与前景[J].推进技术,2010,31(6):660-665. 被引量:45
  • 3刘洋,何国强,刘佩进,李江,吕翔.RBCC组合循环推进系统研究现状和进展[J].固体火箭技术,2009,32(3):288-293. 被引量:27
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二级参考文献69

  • 1陈健,王振国.火箭基组合循环(RBCC)推进系统研究进展[J].飞航导弹,2007(3):36-44. 被引量:9
  • 2王厚庆,何国强,刘佩进.以RBCC为动力的巡航飞行器有效载荷质量敏感性分析[J].固体火箭技术,2007,30(2):87-89. 被引量:4
  • 3刘洋.RBCC引射/亚燃及其模态过渡工作过程研究[D].西安:西北工业大学,2008.
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二级引证文献10

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