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Integral hybrid-boost/solid-fuel ramjet propulsion for lightweight tactical missiles

机译：用于轻型战术导弹的整体混合增压/固体燃料冲压喷气发动机推进

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Approved for public release; distribution is unlimited

机译：批准公开发布；发行是无限的

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作者
Woods Paul C.;
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年度 1995
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原文格式 PDF
正文语种 en_US
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专利

1. Iran unveils new lightweight tactical ballistic missile [J] . Jeremy Binnie Jane's Defence Weekly . 2020,第8期

机译：伊朗推出新型轻型战术弹道导弹
2. Levitating droplets, 3D-printed gun propellants, electromagnetic munitions and a game-changing solid-fuel ramjet [J] . Zevenbergen John F. Aerospace America . 2020,第11期

机译：悬浮液滴，3D印刷枪推进剂，电磁弹药和更换更换的固体燃料拉米特
3. Combustion characteristics of a novel design of solid-fuel ramjet motor with swirl flow [J] . Musa Omer, Chen Xiong, Li Weixuan, Aerospace science and technology . 2019,第SEPa期

机译：一种新型涡流固体燃料冲压发动机的燃烧特性
4. DEVELOPMENT AND TESTING OF THE NAVSEA / ALLIANT TECHSYSTEMS TACTICAL AIRBREATHING PROPULSION, INTEGRAL-ROCKET/RAMJET-ENGINE TEST FACILITY [C] . Gariel D. Randolph, Kenneth W. Beck, Lawrence S. Zajdel, International Symposium on Air Breathing Engines . 2003

机译：Navsea / Alliant TechSystems战术空气灌装推进，积分火箭/拉姆喷嘴 - 发动机测试设施的开发和测试
5. Demonstration of an expert system data base for the surveillance of nuclear weapons and missile technology utilizing a tactical ramjet and missile design as a systems model. [D] . Menges, Pamela A. 1995

机译：演示了使用战术冲压发动机和导弹设计作为系统模型的，用于监视核武器和导弹技术的专家系统数据库。
6. Design and testing of a caseless solid-fuel integral-rocket ramjet engine for use in small tactical missiles. [O] . Fruge Keith J. 1991

机译：用于小型战术导弹的无壳固体燃料整体火箭冲压发动机的设计和测试。

Integral hybrid-boost/solid-fuel ramjet propulsion for lightweight tactical missiles

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