Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX

Low-vulnerability propellants are propellants designed to resist unintended stimuli to increase safety during transport, storage and handling. The substitution of usual nitrocellulose-based gun propellants with these new materials allows maintaining interior ballistics performances while increasing...

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Main Authors: Jordan Ehrhardt, Léo Courty, Philippe Gillard, Barbara Baschung
Format: Article
Language:English
Published: MDPI AG 2020-05-01
Series:Molecules
Subjects:
RDX
Online Access:https://www.mdpi.com/1420-3049/25/10/2276
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spelling doaj-ec1dd65215ca49fb934f2ad54c2fbe0d2020-11-25T02:20:02ZengMDPI AGMolecules1420-30492020-05-01252276227610.3390/molecules25102276Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDXJordan Ehrhardt0Léo Courty1Philippe Gillard2Barbara Baschung3PRISME EA 4229, Université d’Orléans, 18020 Bourges, FrancePRISME EA 4229, Université d’Orléans, 18020 Bourges, FrancePRISME EA 4229, Université d’Orléans, 18020 Bourges, FranceFrench-German Research Institute of Saint-Louis, 68300 Saint-Louis, FranceLow-vulnerability propellants are propellants designed to resist unintended stimuli to increase safety during transport, storage and handling. The substitution of usual nitrocellulose-based gun propellants with these new materials allows maintaining interior ballistics performances while increasing the safety. In this paper, the pyrolysis, ignition and combustion of such propellants are investigated in order to study conditions leading to a safe and reproducible ignition. Low-vulnerability propellants studied are made of different ratios of hexogen (RDX) and nitrocellulose (NC). Three compositions are studied by varying weight percentages of RDX and NC: 95-5, 90-10 and 85-15 for respective weight percentages of RDX-NC. Pyrolysis of these propellants is studied with two different experimental setups: a flash pyrolysis device linked to a gas chromatograph coupled to a mass spectrometer (Py-GC-MS) and a closed-volume reactor coupled to a mass spectrometer. Different molecules, like NO<sub>2</sub>, CO, CH<sub>3</sub>COCH<sub>3</sub> or CH<sub>2</sub>NCH<sub>2</sub>NCH<sub>2</sub>, are obtained during the decomposition of these propellants. Laser ignition of these propellants is studied in a cylindrical closed-volume reactor using a laser diode. Several combustion characteristics, such as ignition delays, maximal overpressures and combustion rates are given for the three propellants using the pressure signals. Moreover, ignition energies are also investigated. Obtained results are compared to the few available literature data. A particular behavior is noticed for the 90-10 propellant. The experimental data collected should serve in the future to have a better understanding of the chemical reactions driving the combustion process of these low-vulnerability propellants.https://www.mdpi.com/1420-3049/25/10/2276pyrolysisignition energycombustion characteristicsRDXnitrocelluloselow-vulnerability propellant
collection DOAJ
language English
format Article
sources DOAJ
author Jordan Ehrhardt
Léo Courty
Philippe Gillard
Barbara Baschung
spellingShingle Jordan Ehrhardt
Léo Courty
Philippe Gillard
Barbara Baschung
Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX
Molecules
pyrolysis
ignition energy
combustion characteristics
RDX
nitrocellulose
low-vulnerability propellant
author_facet Jordan Ehrhardt
Léo Courty
Philippe Gillard
Barbara Baschung
author_sort Jordan Ehrhardt
title Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX
title_short Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX
title_full Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX
title_fullStr Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX
title_full_unstemmed Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX
title_sort experimental study of pyrolysis and laser ignition of low-vulnerability propellants based on rdx
publisher MDPI AG
series Molecules
issn 1420-3049
publishDate 2020-05-01
description Low-vulnerability propellants are propellants designed to resist unintended stimuli to increase safety during transport, storage and handling. The substitution of usual nitrocellulose-based gun propellants with these new materials allows maintaining interior ballistics performances while increasing the safety. In this paper, the pyrolysis, ignition and combustion of such propellants are investigated in order to study conditions leading to a safe and reproducible ignition. Low-vulnerability propellants studied are made of different ratios of hexogen (RDX) and nitrocellulose (NC). Three compositions are studied by varying weight percentages of RDX and NC: 95-5, 90-10 and 85-15 for respective weight percentages of RDX-NC. Pyrolysis of these propellants is studied with two different experimental setups: a flash pyrolysis device linked to a gas chromatograph coupled to a mass spectrometer (Py-GC-MS) and a closed-volume reactor coupled to a mass spectrometer. Different molecules, like NO<sub>2</sub>, CO, CH<sub>3</sub>COCH<sub>3</sub> or CH<sub>2</sub>NCH<sub>2</sub>NCH<sub>2</sub>, are obtained during the decomposition of these propellants. Laser ignition of these propellants is studied in a cylindrical closed-volume reactor using a laser diode. Several combustion characteristics, such as ignition delays, maximal overpressures and combustion rates are given for the three propellants using the pressure signals. Moreover, ignition energies are also investigated. Obtained results are compared to the few available literature data. A particular behavior is noticed for the 90-10 propellant. The experimental data collected should serve in the future to have a better understanding of the chemical reactions driving the combustion process of these low-vulnerability propellants.
topic pyrolysis
ignition energy
combustion characteristics
RDX
nitrocellulose
low-vulnerability propellant
url https://www.mdpi.com/1420-3049/25/10/2276
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