Two curves for selecting general parameters of solid propellant rocket motors

Guozhu Liang; Zhongqin Hang

Two curves for selecting general parameters of solid propellant rocket motors

Guozhu Liang^*
, Zhongqin Hang

^*Corresponding author for this work

Peking University

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

2 Scopus citations

Abstract

The key factors of solid propellant rocket motors design are to choose proper combustion chamber pressure and nozzle expansion ratio. The two parameters are analysed in the view of minimum mass. The two feasible engineering application curves were given in which the curve p_c=f₁(ε), optimum combustion chamber pressure p_c versus nozzle expansion ratio ε versus combustion chamber pressure p_c resolved by iteration method. Therefore, the optimum choice of combustion chamber pressure and nozzle expansion ratio was obtained.

Original language	English
Pages (from-to)	31-34
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	18
Issue number	2
State	Published - Apr 1997
Externally published	Yes

Cite this

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title = "Two curves for selecting general parameters of solid propellant rocket motors",

abstract = "The key factors of solid propellant rocket motors design are to choose proper combustion chamber pressure and nozzle expansion ratio. The two parameters are analysed in the view of minimum mass. The two feasible engineering application curves were given in which the curve pc=f1(ε), optimum combustion chamber pressure pc versus nozzle expansion ratio ε versus combustion chamber pressure pc resolved by iteration method. Therefore, the optimum choice of combustion chamber pressure and nozzle expansion ratio was obtained.",

author = "Guozhu Liang and Zhongqin Hang",

year = "1997",

month = apr,

language = "英语",

volume = "18",

pages = "31--34",

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

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "2",

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TY - JOUR

T1 - Two curves for selecting general parameters of solid propellant rocket motors

AU - Liang, Guozhu

AU - Hang, Zhongqin

PY - 1997/4

Y1 - 1997/4

N2 - The key factors of solid propellant rocket motors design are to choose proper combustion chamber pressure and nozzle expansion ratio. The two parameters are analysed in the view of minimum mass. The two feasible engineering application curves were given in which the curve pc=f1(ε), optimum combustion chamber pressure pc versus nozzle expansion ratio ε versus combustion chamber pressure pc resolved by iteration method. Therefore, the optimum choice of combustion chamber pressure and nozzle expansion ratio was obtained.

AB - The key factors of solid propellant rocket motors design are to choose proper combustion chamber pressure and nozzle expansion ratio. The two parameters are analysed in the view of minimum mass. The two feasible engineering application curves were given in which the curve pc=f1(ε), optimum combustion chamber pressure pc versus nozzle expansion ratio ε versus combustion chamber pressure pc resolved by iteration method. Therefore, the optimum choice of combustion chamber pressure and nozzle expansion ratio was obtained.

UR - https://www.scopus.com/pages/publications/0031119923

M3 - 文章

AN - SCOPUS:0031119923

SN - 1001-4055

VL - 18

SP - 31

EP - 34

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 2

ER -

Two curves for selecting general parameters of solid propellant rocket motors

Abstract

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