Local Temperature Sensitivity Coefficients of a Deterred Spherical Single Base Gun Propellant

• Autorzy: Boulkadid K. , Lefebvre M. H. , Jeunieau L. , Dejeaifve A.

Identyfikatory

DOI

10.22211/cejem/71213

• Języki publikacji: EN

Abstrakty

EN

In our previous investigation, we measured the global temperature sensitivity coefficient of a deterred spherical single base gun propellant following an experimental procedure that did not allows us to determine the local temperature sensitivity coefficients of the deterred and undeterred parts of the investigated propellant. In this paper, we propose an experimental methodology to measure the local temperature sensitivity coefficients of both parts of the spherical deterred gun propellant. This methodology can be summarized as follows: Firstly, we separated the ranges of pressure where the combustion of the deterred and the undeterred parts of the spherical propellant occurs by means of infrared (IR) microscopy measurements. Then the burning rate of the propellant as a function of pressure was calculated according to STANAG 4115 at different initial temperatures. Finally, we determined the local temperature sensitivity coefficients of each part of the spherical propellant.

Słowa kluczowe

EN

initial temperature; temperature sensitivity coefficient; deterred propellant; closed vessel tests; infrared microscopy

• Wydawca: Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
• Czasopismo: Central European Journal of Energetic Materials
• Rocznik: 2017
• Tom: Vol. 14, no. 4
• Strony: 952--965
• Opis fizyczny: Bibliogr. 16 poz., rys., tab.

Twórcy

autor

Boulkadid K.

• UER Chimie Appliquée, Ecole Militaire Polytechnique EMP, BP 17 Bordj El-Bahri, 16046 Algiers, Algeria

autor

Lefebvre M. H.

• Laboratory for Energetic Materials, Royal Military Academy, Av. de la Renaissance 30, 1000 Brussels, Belgium

autor

Jeunieau L.

• Laboratory for Energetic Materials, Royal Military Academy, Av. de la Renaissance 30, 1000 Brussels, Belgium

autor

Dejeaifve A.

• PB Clermont SA, Rue de Clermont 176, 4480 Engis, Belgium

Bibliografia

• [1] Boulkadid, M. K.; Lefebvre, M. H.; Jeunieau, L.; Dejeaifve, A. Temperature Sensitivity of Propellant Combustion and Temperature Coefficients of Gun Performance. Cent. Eur. J. Energ. Mater. 2016, 13(4): 1005-1022.
• [2] 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.
• [3] Assovskii, G.; Zakirov, Z. G.; Leipunskii, O. I. Effect of Ignition on Fuel Combustion. Combust., Expl., Shock Waves (Engl. Transl.) 1983, 19(1): 37-41.
• [4] Leciejewski, Z.; Surma, Z. Effect of Application of Various Ignition Conditions in Closed Vessel Tests on Burning Rate Calculation of a Fine-grained Propellant. Combust., Expl. Shock Waves (Engl. Transl.) 2011, 47(2): 209-216.
• [5] Woodley, C.; Taylor, M.; Wheal, H. Boundary Layer Modelling of the Heat Transfer Process from Igniters to Energetic Materials. Proc. 23rd Int Symp. on Ballistics, Vol. I, Tarragona, Spain 2007, 295-302.
• [6] Khristenko, Yu. F. Experimental Methods for Studying the Combustion of Granular Powder in a Broad Range of Process Parameters. Combust., Expl., Shock Waves (Engl. Transl.) 2001, 27(1): 72-77.
• [7] Definition and Determination of Ballistic Properties of Gun Propellants. STANAG 4115, North Atlantic Council, 1997.
• [8] Fong, C. W. Temperature Sensitivity of Aircraft Cannon Propellants. AFATLTR-82-72, Eglin Airforce Base, FL, Air Force Armament Laboratory, 1982.
• [9] Nguyen, T. T.; Spear R. J. Approaches to Reducing the Temperature Sensitivity of Propulsion Systems for Artillery Ammunition. DSTO Aeronautical and Maritime Research Laboratory, AR No. 008-974, Australia 1994.
• [10] Jeunieau, L.; Lefebvre, M. H.; Dejeaifve, A.; Dobson, R.; Fonder, N. Sensitivity of Nitrocellulose Propellants to the Firing Temperature. 5th Int. Symposium on Energetic Materials and their Applications, Fukuoka, Japan, 12-14 November, 2014.
• [11] Jeunieau, L.; Lefebvre, M. H.; Dejeaifve, A.; Fonder, N.; Guillaume, P.; Boukfessa, H. Centralite Deterred Ball Powder Propellant: Stability and Influence of the Firing Temperature. 2013 Int. Autumn Seminar on Propellants, Explosives and Pyrotechnics, 24-27 September, Chengu, China 2013.
• [12] Jeunieau, L.; Lefebvre, M. H.; Guillaume, P.; Fonder, N. Ballistic Stability and Influence of the Firing Temperature on Deterred Propellants. 2nd Int. Symposium on High Energy Materials, Incheon, South Korea, 17-20 September, 2012.
• [13] Jeunieau, L.; Lefebvre, M. H.; Guillaume, P. Ballistic Stability and Influence of the Firing Temperature of Two Deterred Propellants. 5th Int. Nitrocellulose Symposium, Spiez, Switzerland, 17-18 April, 2012.
• [14] Oberle, W.; White, K. The Application of Electrothermal-Chemical (ETC) Propulsion Concepts to Reduce Propelling Charge Temperature Sensitivity. ARLTR-1509, U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, MD, 1997.
• [15] Clifford, W.; Bertram, K. Ballistic Criteria for Propellant Grain Fracture in the GAU-8/A 30 MM Gun. AFATL-TR-82-21, 1982.
• [16] 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.

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).