| 空天飞机吸气式推进系统/飞行器一体化分析 |
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| 引用本文： | 王占学,屠秋野,陈玉春,唐狄毅.空天飞机吸气式推进系统/飞行器一体化分析[J].推进技术,1997,18(6):10-13. |
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| 作者姓名： | 王占学 屠秋野 陈玉春 唐狄毅 |
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| 作者单位： | 西北工业大学航空发动机系!西安，710072 |
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| 摘 要： | 介绍在进行空天飞机推进系统设计时气动-推进界面的划分和几何参数的选择方法。根据选择的参数进行了小涵道比涡扇发动机和冲压发动机的性能计算，最后给出了空天飞机推进力的计算方法。
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| 关 键 词： | 航天运输系统 航天器推进 飞机-发动机匹配 一体化设计 |
THE ANALYSIS OF AIRBREATHING PROPULSION SYSTEM/VEHICLE INTEGRATION FOR AEROSPACE PLANE |
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| Wang Zhanxue,Tu Qiuye,Chen Yuchun and Tang Diyi.THE ANALYSIS OF AIRBREATHING PROPULSION SYSTEM/VEHICLE INTEGRATION FOR AEROSPACE PLANE[J].Journal of Propulsion Technology,1997,18(6):10-13. |
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| Authors: | Wang Zhanxue Tu Qiuye Chen Yuchun and Tang Diyi |
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| Abstract: | The defination of frame propulsion interface of aerospace plane is introduced. The methods of designing propulsion system and choosing geometry parameters are discribed. According to the chosen parameters, the Performance of a propulsion system is calculated. The algorithm of determining net thrust of aerospace plane is given. |
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| Keywords: | Space transportation system Spacecraft propulsion Airplane-engine matching Integrated design |
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