| 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。 |
| 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 |
| DOI： |
| 分类号:V235 |
| 基金项目: |
|
| THE ANALYSIS OF AIRBREATHING PROPULSION SYSTEM/VEHICLE INTEGRATION FOR AEROSPACE PLANE |
|
Wang Zhanxue,Tu Qiuye,Chen Yuchun,Tang Diyi
|
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Dept. of Aeroengines, Northwestern Polytechnical Univ., Xi’an, 710072
|
| 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. |
| Key words: Space transportation system Spacecraft propulsion Airplane-engine matching Integrated design |
