On the Effectiveness of Using the Real Law of Solid Propellant Burning Rate As a Function of Solid Rocket Motor Pressure

被引：0

作者：

Lipanov, A. M. ^{[1
,2
]}

Kolesnikova, L. N. ^{[2
]}

Leshchev, A. Yu ^{[3
]}

机构：

[1] Russian Acad Sci, Keldysh Inst Appl Math, Moscow 125047, Russia

[2] Kalashnikov Izhevsk State Tech Univ, Izhevsk 426069, Russia

[3] Russian Acad Sci, Udmurt Fed Res Ctr, Ural Branch, Izhevsk 426067, Russia

来源：

COMBUSTION EXPLOSION AND SHOCK WAVES | 2020年 / 56卷 / 02期

关键词：

solid propellant; charge; motor; pressure; burning rate; burning rate law;

D O I：

10.1134/S0010508220020082

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

This paper presents a comparative analysis of the maximum possible solid rocket motor pressures obtained using the exponential and real laws of the propellant burning rate as a function of pressure. It is shown that at high exponents in the burning rate law, there is a large (tens of percent) difference between the maximum motor pressure obtained by the above two methods. In the case where the exponent is in the range 0.3-0.4, the exponential burning rate law overestimates the motor pressure by only 2-3%.

引用

页码：172 / 180

页数：9

共 8 条

[1]

Abugov D. I., 1987, THEORY CALCULATION S

[2]

Bronshtein I. N., 1986, HDB MATH ENG STUDENT

[3] Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure [J].

Lipanov, A. M. .

COMBUSTION EXPLOSION AND SHOCK WAVES, 2017, 53 (05) :569-573

[4] Solid-propellant burning rate as a function of pressure [J].

Lipanov, A. M. .

COMBUSTION EXPLOSION AND SHOCK WAVES, 2013, 49 (03) :283-287

[5]

Lipanov A. M., 1995, DESIGN SOLID ROCKET

[6]

Lipanov A. M., 2007, INTERNAL BALLISTICS

[7]

Sorkin R.E., 1983, Theory of intra-chamber processes in solid fuel rocket systems. Internal ballistics

[8]

Zhegrov E. F., 2011, CHEM TECHNOLOGY DOUB

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