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Journal ArticleDOI

Role of Binders in Solid Propellant Combustion

Norman S. Cohen, +2 more
- 01 Feb 1974 - 
- Vol. 12, Iss: 2, pp 212-218
TLDR
In this article, the effects of inert binder properties on composite solid propellant burning rate were investigated and defined for many binders of practical interest over a wide range of heating rates and pressures, in several environmental gases, with and without 10 percent ammonium perchlorate (AP) contained in the sample, and in some cases with catalysts.
Abstract
: The objective of this program was to investigate and define the effects of inert binder properties on composite solid propellant burning rate. Experimental pyrolysis data were obtained for many binders of practical interest over a wide range of heating rates and pressures, in several environmental gases, with and without 10-percent ammonium perchlorate (AP) contained in the sample, and in some cases with catalysts. These data were used to extract kinetics constants from Arrhenius plots, and heat of decomposition. In addition, motion pictures were taken of the pyrolyzing surface and gas samples were extracted for analysis. Pyrolysis kinetics varied between binders, but were found to be independent of pressure, the presence of AP, and the presence of burn rate catalysts; however, a chlorine gas environment had a material effect upon the results. All of the binders exhibited molten, boiling surfaces mingled with char, to varying degrees; the amount of char increased with AP present, and in chlorine. Relevant data were input to the Derr-Beckstead-Price combustion model in order to associate binder properties with known binder effects on burning rate. Although the effects were predictable, they stemmed from properties other than pyrolysis kinetics; however, the binder data as applied to the model revealed possible deficiencies in the model, which are discussed. It appears that the approach of combustion tailoring by binder modification would have to involve the gas phase combustion processes rather than surface pyrolysis. Therefore, future work concerning the role of binder should be directed toward the gas phase.

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Citations
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Journal ArticleDOI

Catalytic effects of nano additives on decomposition and combustion of RDX-, HMX-, and AP-based energetic compositions

TL;DR: In this paper, the effects of nano-sized additive on decomposition kinetics, reaction models, decomposition mechanisms and burning rates, pressure exponents, combustion wave structures, and flame propagation of RDX-, HMX-, and AP-based energetic compositions are discussed.
Journal ArticleDOI

Regression Rate Behavior of Hybrid Rocket Solid Fuels

TL;DR: In this paper, an experimental investigation of the regression-rate characteristics of hydroxyl-terminated polybutadiene (HTPB) solid fuel burning with oxygen was conducted using a windowed, slab-geometry hybrid rocket motor.
Book

Solid propellant chemistry, combustion, and motor interior ballistics

TL;DR: In this article, the authors present in-depth coverage on a wide range of topics including advanced materials and non-traditional formulations; the chemical aspects of organic and inorganic components in relation to decomposition mechanisms, kinetics, combustion and modelling; safety issues, hazards and explosive characteristics; and experimental and computational interior ballistics research, including chemical information and the physics of the complex flow field.
Journal ArticleDOI

Probing the Reaction Mechanism of Aluminum/Poly(vinylidene fluoride) Composites.

TL;DR: This work examines the PIR between alumina and PVDF to further explain the reaction mechanism of the Al/PVDF system and shows a direct correlation between the amount of alumina in the PVDF film and the relative signal intensity of hydrogen fluoride release (HF).
Journal ArticleDOI

A Model of AP/HTPB Composite Propellant Combustion in Rocket-Motor Environments

TL;DR: In this article, a comprehensive theoretical/numerical model for treating AP/HTPB composite-propellant combustion in a rocket-motor environment is presented, which takes into account the conservation equations in both the gas and condensed phases, and accommodates finite-rate chemical kinetics and variable thermophysical properties.
References
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Journal ArticleDOI

A model of composite solid-propellant combustion based on multiple flames

TL;DR: In this paper, a model describing the combustion of ammonium perchlorate (AP) composite propellants has been developed based on a flame structure surrounding individual oxidizer crystals; the relationship between crystals and the binder matrix was evaluated statistically.
Journal ArticleDOI

Mechanism of the decomposition of ammonium perchlorate

TL;DR: In this paper, a detailed mechanism for the chemical decomposition of ammonium perchlorate is proposed, which is adaptable to a wide range of conditions; to the low-temperature decomposition, to combustion, to the catalysed decomposition and to decomposition under various reactive gases.
Proceedings ArticleDOI

A detailed model of the combustion of composite solid propellants

C. Hermance
TL;DR: In this paper, a model for the steady state combustion of composite solid propellants is presented, which consists of a detailed combination of the steady-state decomposition process of the fuel and oxidizer, taking into account the oxidizer particle size distribution.
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