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The Applicability of Chromatographic Methods in the Investigation of Ageing Processes in Double Base Rocket Propellants

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The ageing of double base (DB) rocket propellants is the result of chemical decomposition reactions and physical processes, causing degradation of a number of relevant propellant properties (such as reduction in stabilizer and nitroglycerine (NG) content, reduction of the mean molecular mass of nitrocellulose (NC) etc.), which is refected in a decrease in the reliable service life time of DB propellants. This is the reason why the study of processes of ageing and their consequences (effects) is so important. In this paper we have studied the kinetics of DB rocket propellant decomposition during their artifcial ageing, i.e. at elevated temperatures. The kinetic parameters were obtained by measurements of the stabilizer/Ethyl Centralite (EC) content and the mean molecular mass reduction of NC, during artifcial ageing at temperatures of 80, 85 and 90 °C. Consumption of the EC was observed using High Performance Liquid Chromatography (HPLC), whilst the reduction in the mean molecular mass of NC was monitored using Gel Permeation Chromatography (GPC). It has been shown that artifcial ageing of DB propellant causes signifcant EC consumption and a reduction in the mean molecular mass of NC, from the very beginning of ageing. EC is entirely consumed after 120 days at 80 °C, and is followed by the intensive reactions of NC decomposition. Signifcant changes in the mean molecular mass of NC starts after 60 days of ageing at 90 °C (or ~250 days at 80 °C). The results obtained from the kinetic data have shown that the activation energy of DB propellant decomposition, determined on the basis of changes in the mean molecular mass of NC is 145.09 kJ•mol-1 , whilst the activation energy of decomposition obtained on the basis of EC consumption is 142.98 kJ•mol-1 , which is consistent with available literature values [1, 2].
Rocznik
Strony
245--262
Opis fizyczny
Bibliogr. 19 poz., rys., tab.
Twórcy
  • Brodarski Institute, Ave.V. Holjevca 20, HR-10020 Zagreb, Croatia
autor
  • Nanyang Technological University, Energetics Research Institute, Singapore
autor
  • Ministry of Defense, Zagreb, Croatia
Bibliografia
  • [1] Volk F., Bohn M.A., Wunsch G., Determination of Chemical and Mechanical Properties of Double Base Propellants During Ageing, Propellants Explos. Pyrotech., 1987, 12, 81-87.
  • [2] Bohn M.A., Volk F., Ageing Behavior of Propellants Investigated by Heat Generation, Stabilizer Consumption and Molar Mass Degradation, Propellants Explos. Pyrotech., 1992, 17, 171.
  • [3] Bohn M.A., Kinetic Modelling of the Ageing of Gun and Rocket Propellants for the Improved and Time-Extend Prediction of Their Service Lifetime, Proc. 1998, Life Time Cycles of Energetic Materials, Fullerton, California, USA, 1998.
  • [4] Volk F., Bohn M.A., Ageing Behaviour of Propellants Determined by Mass Loss, Heat Generation, Stabiliser Consumption, and Molar Mass Decrease, 87th Symp., Propulsion and Energetic Panel (PEP) of the AGARD, ‘Service Life of Solid Propellant Systems’, Athens, Greece, 1996.
  • [5] Volk F., Wunsch G., Determination of the Decomposition Behavior of Double-Base Propellants at Low Temperatures, Propellants Explos. Pyrotech., 1985, 10, 181.
  • [6] Pfeil A., Krause H.H., Eisenreich N., The Consequences of Beginning Slow Thermal Decomposition on the Molecular Weight of Nitrated Cellulose, Thermochim. Acta, 1985, 85, 395.
  • [7] Bohn M.A., Volk F., Prediction of the Lifetime of Propellants by Stabilizer Consumption and Molar Mass Decrease, Proc., ADPA Predictive Technology Symp., New Jersey, USA, 1993.
  • [8] Vogelsanger B., Chemical Stability, Compatibility and Shelf Life of Explosives, Chimia, 2004, 58, 401.
  • [9] Merzhanov A.G., Abramov V.G., Thermal Explosion of Explosives and Propellants. A Review, Propellants and Explosives, 1981, 6, 130.
  • [10] Volk F., Determining the Shelfife of Solid Propellants, Propellants Explos. Pyrotech., 1976, 1, 59-65.
  • [11] Volk F., Determination of the Lifetimes of Gun Propellants Using Thin-layer Chromatography, Propellants Explos. Pyrotech., 1976, 1, 90-97.
  • [12] Tompa A.S., Thermal Analysis of Liquid and Solid Propellants, J. Hazard. Mater., 1980, 4, 95-112.
  • [13] Lurie B., Kinetics and Mechanism of the Single and Double Base Propellant Decomposition at Relatively Low Temperatures, 24th Int. Annu. Conf. of ICT, Karlsruhe, Germany, 1993, 57, p. 1.
  • [14] Rodante F., A ‰ Thermoanalytical Study of the Decomposition of a Double-base Propellant, Thermochim. Acta, 1986, 101, 373.
  • [15] Bauer C.L., Deacon P.R., Garman R.N., Emsley A.M., Jones J.R., Low Temperature Non-Isothermal Ageing of Nitrocellulose, Propellants Explos. Pyrotech., 2005, 30, 231.
  • [16] NATO Allied Ordnance Publication (AOP-48).
  • [17] Matečić Mušanić S., Sućeska M., Čuljak R., Study of Ageing Processes of Double Base Rocket Propellants, Based on Stabilizer Consumption, New Trends Res. Energ. Mater., Proc. Semin., 15th, Pardubice, Czech Republic, 2012, 724-734.
  • [18] Bamford C.H., Tipper C.F.H., Comprehensive Chemical Kinetics, Reactions in the Solid State, vol. 22, Elsevier Scientifc Publishing Company, New York, 1980.
  • [19] Janović Z., Polimerizacije i polimeri, HDKI, Zagreb, 1997.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-28dfd079-4f4f-4a29-bd93-3d5fe1ac9150
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