The analysis of airbreathing propulsion system/vehicle integration for aerospace plane

Zhanxue Wang; Qiuye Tu; Yuchun Chen; Diyi Tang

The analysis of airbreathing propulsion system/vehicle integration for aerospace plane

Zhanxue Wang, Qiuye Tu, Yuchun Chen, Diyi Tang

School of Power and Energy

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

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.

Original language	English
Pages (from-to)	10-13
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	18
Issue number	6
State	Published - 1997

Keywords

Airplane-engine matching
Integrated design
Space transportation system
Spacecraft propulsion

Cite this

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title = "The analysis of airbreathing propulsion system/vehicle integration for aerospace plane",

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.",

keywords = "Airplane-engine matching, Integrated design, Space transportation system, Spacecraft propulsion",

author = "Zhanxue Wang and Qiuye Tu and Yuchun Chen and Diyi Tang",

year = "1997",

language = "英语",

volume = "18",

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AU - Wang, Zhanxue

AU - Tu, Qiuye

AU - Chen, Yuchun

AU - Tang, Diyi

PY - 1997

Y1 - 1997

N2 - 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.

AB - 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.

KW - Airplane-engine matching

KW - Integrated design

KW - Space transportation system

KW - Spacecraft propulsion

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M3 - 文章

AN - SCOPUS:0031293518

SN - 1001-4055

VL - 18

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JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 6

ER -

The analysis of airbreathing propulsion system/vehicle integration for aerospace plane

Abstract

Keywords

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