This article is cited in 1 paper

Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure

A. M. Lipanov

Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, 125047, Russia

Abstract: Five variants of calculating the burning rate of a solid propellant as a function of the pressure in a solid-propellant rocket motor are considered. Two variants of analytical expressions are proposed for approximating real dependences. In all variants, the pressure in the rocket motor can be presented by simple analytical expressions as a function of solid propellant parameters, charging conditions, and structural factors of the charge and motor.

Keywords: solid propellant, burning rate, rocket motor.

UDC: 621.454.3

Received: 30.11.2016
Revised: 26.12.2016

DOI: 10.15372/FGV20170510

 English version: Combustion, Explosion and Shock Waves, 2017, 53:5, 569–573

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