Effects of control flow parameters on vortex valve SRM thrust modulation

Xiang Geng Wei; Guo Qiang He; Jiang Li; Jian Chen; Xiao Jing Yu

Effects of control flow parameters on vortex valve SRM thrust modulation

Xiang Geng Wei
, Guo Qiang He
, Jiang Li
, Jian Chen
, Xiao Jing Yu

航天学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

The effects of pressure, mass flow rate, velocity and temperature of control flow on the performance of thrust modulation in vortex valve SRM were studied experimentally and numerically. It shows that the increase of the temperature, mass flow rate and velocity of the control flow can all increase the thrust modulation ratio.

源语言	英语
页（从-至）	571-575
页数	5
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	30
期	5
出版状态	已出版 - 10月 2009

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@article{7c1a10db1de64a208ee5038fcaca9d72,

title = "Effects of control flow parameters on vortex valve SRM thrust modulation",

abstract = "The effects of pressure, mass flow rate, velocity and temperature of control flow on the performance of thrust modulation in vortex valve SRM were studied experimentally and numerically. It shows that the increase of the temperature, mass flow rate and velocity of the control flow can all increase the thrust modulation ratio.",

keywords = "Numerical simulation, Rocket engine with variable thrust, Solid propellant rocket motor, Thrust modulation, Vortex valve",

author = "Wei, \{Xiang Geng\} and He, \{Guo Qiang\} and Jiang Li and Jian Chen and Yu, \{Xiao Jing\}",

year = "2009",

month = oct,

language = "英语",

volume = "30",

pages = "571--575",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "Journal of Propulsion Technology",

number = "5",

}

TY - JOUR

T1 - Effects of control flow parameters on vortex valve SRM thrust modulation

AU - Wei, Xiang Geng

AU - He, Guo Qiang

AU - Li, Jiang

AU - Chen, Jian

AU - Yu, Xiao Jing

PY - 2009/10

Y1 - 2009/10

N2 - The effects of pressure, mass flow rate, velocity and temperature of control flow on the performance of thrust modulation in vortex valve SRM were studied experimentally and numerically. It shows that the increase of the temperature, mass flow rate and velocity of the control flow can all increase the thrust modulation ratio.

AB - The effects of pressure, mass flow rate, velocity and temperature of control flow on the performance of thrust modulation in vortex valve SRM were studied experimentally and numerically. It shows that the increase of the temperature, mass flow rate and velocity of the control flow can all increase the thrust modulation ratio.

KW - Numerical simulation

KW - Rocket engine with variable thrust

KW - Solid propellant rocket motor

KW - Thrust modulation

KW - Vortex valve

UR - https://www.scopus.com/pages/publications/70749103993

M3 - 文章

AN - SCOPUS:70749103993

SN - 1001-4055

VL - 30

SP - 571

EP - 575

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 5

ER -

Effects of control flow parameters on vortex valve SRM thrust modulation

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