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Tytuł artykułu

Statistical Approach in Determining Energy Ballistic Parameters of Gunpowder Contained in the 7.62×39 mm Ammunition Based on Measuring the Development of Pressure in a Manometric Bomb

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Currently, most design processes are carried out with the use of specialized tools in the form of advanced computer programs. Assuming that mathematical models are formulated without significant simplifications and their numerical solution is performed with high accuracy, the quality of the problem solution is determined each time by the input data. In the case of the main problem of internal ballistics, these will be the reliably obtained energy-ballistic values of the gunpowder. In the present work, classical methodology for determining the energy-ballistic parameters of gunpowder based on the recorded pressure curve in a manometric bomb was implemented using mathematical statistics. For the assumed distribution of the probability function, which is the Student’s t-distribution, confidence intervals have been established for the assumed confidence level for the values of the parameters of the distribution of ballistic features, such as the loading density power, gunpowder force, covolume and proper burn rate. These parameters were determined for three different gunpowder charges contained in the cal. 7.62x39 mm ammunition: SM FMJ 8 g, Barnaul FMJ 123gr 8.1 g ZN FMJ and STV FMJ-CIP 8gr/123grs.
Rocznik
Strony
260--283
Opis fizyczny
Bibliogr. 18 poz., rys., tab., wykr.
Twórcy
  • Faculty of Mechanical and Industrial Engineering, Institute of Mechanics and Printing, Department of Mechanics and Weaponry Technology, Warsaw University of Technology, 85 Narbutta Str., 02-524 Warsaw, Poland
Bibliografia
  • [1] Grys, S.; Trzciński, W.A. Calculation of Combustion Parameters for Gun Propellants. Arch. Combust. 2011, 11(1-2): 3-20.
  • [2] Leugelle, G.; Duterque, J.; Trubert, J.F. Combustion of Solid Propellants. RTO/VKI Special Course on Internal Aerodynamics in Solid Rocket Propulsion, RTOEN-023, Rhock-Saint-Genese, Belgium, 2004.
  • [3] Michalski, J.; Janiszewski, J.; Leciejewski, Z.; Pichola, W.; Surma, Z. Closed Vessel Equipped with Capillary Plasma Generator as the New Method of Propellant’s Ignition and Pirostatic Investigation. Mater. Wysokoenerg. (High Energy Mater.) 2012, 4: 21-26.
  • [4] Michalski, J.; Leciejewski, Z. Closed Vessel Investigation of Propellant Ignition Process with Using Capillary Plasma Generator. Problems of Mechatronics. Armament, Aviation, Safety Engineering 2015, 6: 19-26; https://doi.org/10.5604/20815891.1149753.
  • [5] Torecki, S. Internal Ballistics. (in Polish) Warsaw: Military University of Technology, 1980.
  • [6] Trębiński, R.; Janiszewski, J.; Leciejewski, Z.; Surma, Z.; Kamińska, K. On Influence of Mechanical Properties of Gun Propellants on Their Ballistic Characteristics Determined in Closed Vessel Tests. Materials 2020, 13(14): paper 3243; https://doi.org/10.3390/ma13143243.
  • [7] STANAG 4115, Edition 2, Definition and Determination of Ballistic Properties of Gun Propellants. Military Agency for Standardization, 1997.
  • [8] Wrzesiński, Z. Internal Ballistics of Classical Barrel Weapons. (in Polish) Warsaw: Oficyna Wydawnicza Politechniki Warszawskiej, 2018; ISBN 978-83-7814-774-9.
  • [9] Mukhtar, A.; Nasir, H. Comparative Closed Vessel Firing-Ballistic Parameters Evaluation for Development of Base Bleed Composite Solid Propellant. Engineering, Technology & Applied Science Research 2018, 8(6): 3545-3549; https://doi.org/10.48084/etasr.2370.
  • [10] Gańczyk-Specjalska, K.; Cieślak, K.; Zembrzucka, K. Thermal Properties of Modified Single-base Propellants. Mater. Wysokoenerg. (High Energy Mater.) 2021, 13: 21-26; https://doi.org/10.22211/matwys/0212.
  • [11] Trebiński, R.; Leciejewski, Z.; Surma, Z.; Fikus, B. Analysis of Dynamic Vivacity Curves Obtained on the Basis of Valved Closed Vessel Test Data. DEStech Publications, Inc., 2017, https://doi.org/10.12783/ballistics2017/16824.
  • [12] Leciejewski, Z.K. Experimental Study of Possibilities for Employment of Linear Form of Burning Rate Law to Characterise the Burning Process of Fine-Grained Propellants. Cent. Eur. J. Energ. Mater. 2008, 5(1): 45-61.
  • [13] Leciejewski, Z.K. Criticism of Linear Form of Burning Rate Law with Reference to Conventional Fine-Grained Propellants. Biul. Wojsk. Akad. Tech. (Bull. Mil. Univ. Technol.) 2008, 57(3): 61-72.
  • [14] Carlucci, D.E.; Jacobson, S.S. Ballistics: Theory and Design of Guns and Ammunition. CRC Press, 2018; ISBN 9781315165967.
  • [15] Leciejewski, Z.K.; Surma, Z.; Zuk, P. Factors Determining Nature of Dynamic Vivacity Curve During Closed Vessel Investigations. DEStech Publications, Inc., 2017, https://doi.org/10.12783/ballistics2017/16836.
  • [16] Grune, D. The Influence of the Variation of Combustion Chamber Volume Under Pressure Load on the Determinational of Thermodynamic Characteristics of Solid Propellants in Pressure Bombs. Propellants Explos. Pyrotech. 1987, 12(1): 8-12; https://doi.org/10.1002/prep.19870120103.
  • [17] Celminš, A. Solid Propellant Burning Rate Measurement in a Closed Bomb. Combust.Flame 1974, 23: 381-397; https://doi.org/10.1016/0010-2180(74)90121-7.
  • [18] Wrzesiński, Z. Measurement Uncertainty in Laboratory Tests. (in Polish) Warsaw, 2023; ISBN 978-83-8156-497-7.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-6952f309-9515-4d83-8628-d014acf62f11
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