RUS  ENG
Full version
JOURNALS // Fizika Goreniya i Vzryva // Archive

Fizika Goreniya i Vzryva, 2013 Volume 49, Issue 1, Pages 62–73 (Mi fgv9)

This article is cited in 11 papers

Combustion mechanism of RDX and HMX and possibilities of controlling the combustion characteristics of systems based on them

V. A. Strunin, L. I. Nikolaeva

Institute of Problems of Chemical Physics, Russian Academy of Sciences, Chernogolovka, 142432, Russia

Abstract: Modeling of the combustion of cyclic nitramines (CNAs) has shown that their combustion proceeds by the same mechanism with the joint effect of the processes in the condensed and gas phases. The combustion characteristics of the pure substances can be changed only at low pressures by using catalysts acting in the condensed phase, and at high pressures, this problem is difficult to solve. The combustion of binary compositions [CAN + fuel (F), CAN + ammonium perchlorate (AP)] and ternary compositions (AP + CAN + F) is considered. It is shown that the combustion mechanism and characteristics are determined by the chemical interaction and heat exchange between the reactants, which depend on the characteristic particle size in the system.

Keywords: solid rocket propellant, RDX, HMX, modeling, combustion mechanism, control of combustion characteristics.

UDC: 536.46

Received: 06.07.2011


 English version:
Combustion, Explosion and Shock Waves, 2013, 49:1, 53–63

Bibliographic databases:


© Steklov Math. Inst. of RAS, 2024