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High‐Pressure Combustion Studies of Energetic Materials

- pp 47-67
TLDR
In this paper , the importance of visually observing the combustion process is used to explain slope breaks that appear in the pressure-dependent burning rates of liquid propellants, which are not predicted by current models.
Abstract
Pressure plays a significant role in determining the burning rate of a propellant. Experimental measurements of burning rates are essential for quantifying their magnitudes and defining their functional behavior with pressure, as predictive capabilities from theory and modeling are still not sufficient. Performing measurements over a wide range of conditions including extreme conditions and visually observing the combustion process are beneficial to the fundamental understanding of anomalies in burning rate behavior and to the development of models. There are various methods to measure burning rates, but visual observations have rarely been made above 7 MPa. In this chapter, high-pressure visually aided experiments and burning rate measurements of liquid and solid propellants are discussed and reviewed. The importance of visually observing the combustion process is used to explain slope breaks that appear in the pressure-dependent burning rates of liquid propellants, which are not predicted by current models. The reasons for these breaks can be due to physical and chemical phenomena, and in many cases, the measurements are not representative of fundamental intrinsic rates.

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References
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Journal ArticleDOI

Burning Rate of Solid Propellant Ingredients, Part 1: Pressure and Initial Temperature Effects

TL;DR: Burning rate data for three compounds that are currently used in propellant and explosive formulations are presented in this article with respect to initial temperature and pressure, and the dependence of burning rate on initial temperature is investigated for ammonium perchlorate, HMX, and RDX.
Journal ArticleDOI

HMX and RDX - Combustion mechanism and influence on modern double-base propellant combustion

TL;DR: In this paper, the burning wave structures of double-base propellants (DBF) containing HMX and various catalysts were used to establish the influence of additional nitramines on the unified dependencies of simple DBFs.
Journal ArticleDOI

Analysis of RDX Monopropellant Combustion with Two-Phase Subsurface Reactions

TL;DR: In this article, a comprehensive numerical analysis has been developed to study the key physicochemical processes involved in the self-sustained combustion of 1,3,5-trinitr ohexahydro-s-triazine (RDX) monopropellant.
Journal ArticleDOI

Deflagration rate, surface structure, and subsurface profile of self-deflagrating single crystals of ammonium perchlorate

T. L. Boggs
- 01 May 1970 - 
TL;DR: In this article, a single crystal self-deflagration of pure ammonium perchlorate single crystal was studied, determining energy transfer mechanisms from pressure effects, combustion characteristics and subsurface profile.
Journal ArticleDOI

Combustion of ammonium perchlorate

J.D. Hightower, +1 more
TL;DR: In this paper, the authors used cleaved sections of large single crystals grown from water solution, discussing burning rate and combustion zone, and discussed burning area and burning rate of ammonium perchlorate.
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