| 固体火箭-冲压发动机的研究进展 |
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| 引用本文： | 戴耀松.固体火箭-冲压发动机的研究进展[J].推进技术,1987,8(5):40-45,78. |
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| 作者姓名： | 戴耀松 |
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| 摘 要： | 固体火箭-冲压发动机兼有火箭发动机和冲压发动机的优点,它结构简单,能量高,可靠性好,非常适合于军事用途,具有广阔的应用前景.本文详细地讨论了这类推进系统及其主要组件的技术发展状况、贫氧推进剂、燃料流量控制、冲压燃烧室、助推和转级等技术,还讨论了将来的应用和研制发展的方向.
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| 关 键 词： | 冲压式喷气发动机 固体火箭发动机 贫氧富燃料推进剂 技术 应用 |
Advances in Solid Rocket-Ramjet Engine |
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| Dai Yaosong.Advances in Solid Rocket-Ramjet Engine[J].Journal of Propulsion Technology,1987,8(5):40-45,78. |
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| Authors: | Dai Yaosong |
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| Institution: | Dai Yaosong |
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| Abstract: | This paper reviewed the lastest development of solid rocket-ramjet engine in the area of lean-oxygen propellant, fuel control, ramjet combustor, boosting and conversion technology etc in great details. Its future development and application are also discussed. |
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| Keywords: | Ramjet Solid rocket engine Oxygen poor rich-fuel propellant Technology Application |
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