| 整体式固体火箭冲压发动机研制 |
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| 引用本文： | 张家骅,胡顺楠,顾炎武,曹中俄.整体式固体火箭冲压发动机研制[J].推进技术,1998,19(2):10-14. |
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| 作者姓名： | 张家骅 胡顺楠 顾炎武 曹中俄 |
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| 作者单位： | 航天工业总公司31所,北京,100074 |
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| 摘 要： | 概要介绍了我国第一种整体式固体火箭冲压发动机试验研究样机的研制，讨论了样机地面试验研究和飞行试验研究两大阶段中，整机（含主级和助推级）各部件及分系统的设计，试制和试验工作，样机结合合理，主级比冲比国外同类型号导弹发动机有较大提高，助推级综合性能和热防护也优于后者。
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| 关 键 词： | 冲压发动机 推进系统 固体火箭发动机 |
DEVELOPMENT OF AN INTEGRAL SOLID ROCKET RAMJET ENGINE |
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| Zhang Jiahu,Hu Shunnan,Gu Yanwu and Cao Zhong.DEVELOPMENT OF AN INTEGRAL SOLID ROCKET RAMJET ENGINE[J].Journal of Propulsion Technology,1998,19(2):10-14. |
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| Authors: | Zhang Jiahu Hu Shunnan Gu Yanwu and Cao Zhong |
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| Institution: | The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074 |
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| Abstract: | An integral solid rocket ramjet engine in China is introduced.The design,manufacture and test of the whole engine(both sustainer and booster),components and sub systems during ground and flight test phases were described.The test results show that this prototype was reasonable,the specific impulse of cruise stage was higher than that similar to engines abroad,and the integrated booster performance and thermal protection technique were satisfactory |
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| Keywords: | Integral rocket ramjet Engine design Propulsion system test |
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