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Temperature Sensitivity of Propellant Combustion and Temperature Coefficients of Gun Performance

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
One of the objectives of gun propellant research is to develop green formulations of gunpowder that should be less temperature sensitive than the current gun propellant. The temperature sensitivity of these new green formulations of the propellant should be measured to identify the less temperature sensitive green formulations. However, there are deficiencies in the methodologies for the measurement of the temperature sensitivity of gun propellants. Therefore, the aim of this investigation was to fill the gap by establishing a method for the measurement of the temperature sensitivity of deterred gun propellants by closed vessel tests. The temperature sensitivity of the burning rate of ball propellants and the temperature coefficients of gun performance were determined using closed vessel tests and ballistic firing, respectively. Specific definitions of temperature sensitivity and temperature coefficients were evaluated. The relation between these parameters has never been explicitly investigated previously. Assessing the temperature sensitivity of propellants by closed vessel tests is of added value to the range of ballistic tests if the results of these tests can be well correlated to the results of ballistic firings. Therefore, a comparison between both parameters was made. A correspondence has been observed between the temperature sensitivity of the propellant burning rate, as obtained from closed vessel tests, and the temperature coefficients as obtained from ballistic firings.
Rocznik
Strony
1005--1022
Opis fizyczny
Bibliogr. 8 poz., rys., tab.
Twórcy
  • Laboratory of Energetic Materials, Royal Military Academy, Av. de la Renaissance 30 1000 Brussels, Belgium
  • Laboratory of Energetic Materials, Royal Military Academy, Av. de la Renaissance 30 1000 Brussels, Belgium
autor
  • Laboratory of Energetic Materials, Royal Military Academy, Av. de la Renaissance 30 1000 Brussels, Belgium
autor
  • PB Clermont SA, Rue de Clermont 176, 4480 Engis, Belgium
Bibliografia
  • [1] Manning T.G., Thompson D., Ellis M., Lieb R., Leadore M., Colburn J., Homan B.E., Worrell D.A., Moran K.B., Ritchie S.J., Environmentally Friendly Green Propellant for the Medium Caliber Training Rounds, U.S. Army TACOMARDEC Picatinny Arsenal Picatinny, NJ 07806-5000, 2006.
  • [2] Oberle W., White K., The Application of Electrothermal-Chemical (ETC) Propulsion Concepts to Reduce Propelling Charge Temperature Sensitivity, ARL-TR-1509, U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, MD, 1997.
  • [3] Tarn T.N., Robert J.S., Approaches to Reducing the Temperature Sensitivity of Propulsion Systems for Artillery Ammunition, DSTO-TR-0102, 1994.
  • [4] STANAG 4115 (Edition 2): Definition and Determination of Ballistic Properties of Gun Propellants, North Atlantic Council, 1997.
  • [5] Clifford W., Temperature Sensitivity of Aircraft Cannon Propellants, AFATLTR-82-72, 1982.
  • [6] Jeunieau L., Lefebvre M.H., Guillaume P., Quantitative Infra-red Microscopy Method for the Determination of the Deterrent Diffusion Activation Energy in a Spherical Propellant, Cent. Eur. J. Energ. Mater., 2007, 4, 109-124.
  • [7] Jeunieau L., Lefebvre M.H., Guillaume P., Characterization of Deterred Propellants by Closed Vessel Tests: Importance of the Ignition Method, Cent. Eur. J. Energ. Mater., 2005, 2, 39-53.
  • [8] Jeunieau L., Lefebvre M.H., Guillaume P., Wilker S., Chevalier S., Stability Analyses of Rolled Ball Propellants, Part III – Correlation between Closed Vessel Tests, Ballistic Firing and Deterrent Migration, 36th Int. Annu. Conf. ICT, Karlsruhe, 2005, 14.
Uwagi
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-0586cf38-84fd-47e1-8ae8-027b56a1fb85
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