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Comparison of Different Propulsive Systems for Air-Breathing Launcher

机译：空气呼吸发射器不同推进系统的比较

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Several concepts of propulsive systems fitted on a SSTO launcher have been studied within the frame of French PREPHA program: -turborocket/scramjet/rocket, -turbojet with reheat/rajet/scramjet/rocket, -rocket/ramjet/scramjet/rocket, -air-ejector rocket/ramjet/scramjet/rocket.

机译：在法式普雷弗计划的框架内研究了拟合在SSTO发射器上的推进系统的几种概念：-Turborocket / Scramjet / Rocket，-Turbojet配有再热/ Rajet / Scramjet / Rocket，-Rocket / Ramjet / Scramjet / Rocket，-Air -ejector火箭/拉姆喷嘴/瘙痒液/火箭。

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《AIAA international aerospace planes and hypersonics technologies conference 》|1995年||共9页
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M.Lepelletier; R.Zendron; P.Bellande; D.Scherrer; B.Forrat;
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中图分类飞机构造与设计 ;
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4. Comparison of Different Propulsive Systems for Air-Breathing Launcher [C] . M.Lepelletier, R.Zendron, P.Bellande, AIAA international aerospace planes and hypersonics technologies conference . 1995

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Comparison of Different Propulsive Systems for Air-Breathing Launcher

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