| 火箭冲压发动机无喷管助推器分析 |
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| 引用本文： | 曹任刚,郭颜红.火箭冲压发动机无喷管助推器分析[J].战术导弹技术,2011(3):48-53. |
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| 作者姓名： | 曹任刚 郭颜红 |
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| 作者单位： | 中国空空导弹研究院; |
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| 摘 要： | 介绍了无喷管固体火箭发动机性能计算的基本架设、控制方程和装药燃速的处理，对影响无喷管助推器性能设计的火箭冲压发动机主要要求、影响进行了分析，围绕装药长度、冲压喷管尺寸、推力要求等设计约束条件对无喷管助推器设计的影响进行了分析与计算，给出定量计算结果和研究结论．同时，介绍了一种提高火箭；中压发动机无喷管助推器性能的新方法、新方案：冲压喷管共用结构方案．
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| 关 键 词： | 助推器 无喷管火箭发动机 火箭冲压发动机 |
Analysis on Nozzleless Booster of Rocket Ramjet Engine |
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| Cao Rengang,Guo Yanhong.Analysis on Nozzleless Booster of Rocket Ramjet Engine[J].Tactical Missile Technology,2011(3):48-53. |
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| Authors: | Cao Rengang Guo Yanhong |
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| Affiliation: | Cao Rengang,Guo Yanhong(China Air-to-Air Missile Academy,Luoyang Henan471009,China) |
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| Abstract: | The basic structure,control equation and charge combustion speed processing in calculating performances of nozzleless solid rocket motor are presented.According to nozzleless booster design,the relative requirement for rocket-ramjet engine is analyzed.The constraints on nozzleless booster design are analyzed and calculated,including charge capacity,ramjet nozzle size,thrust etc,to obtain a quantitative result and research conclusion.A shared ramjet-nozzle structure is proposed as a new concept for improving... |
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| Keywords: | booster nozzleless rocket motor rocket ramjet engine |
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