PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Closed vessel equipped with capillary plasma generator as the new method of propellant’s ignition and pirostatic investigation

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Contemporary development of new types of ammunition is concentrated to improve the energetic characteristics, chemical stability and operational safety of propellants. Response to this requests are low vulnerability (LOVA) propellants. Previous closed vessel investigations indicated that classical primers (electric or percussion with black powder bedding) when used with LOVA propellants causes unstable burning, defagration or even lack of ignition. Plasma generators, which create higher energy fux, temperature and make possible to control combustion process are possible solution of this problem. Assuming that in the future Poland may be a manufacturer of LOVA propellants, Military University of Technology began to develop of new closed vessel equipped with capillary plasma generator (CPG) - the new method of low vulnerability propellants ignition. In CPG systems plasma generation is obtained by discharge of high power capacitors through low diameter conductors in polyethylene coating (mainly cooper, aluminium and tungsten wires), causing them to explode (or other metallic vapour generating device). After wire explosion plasma causes burning of polyethylene, giving additional energy to plasma cloud. Plasma is vented to vessel causing high energy and heat fux through radiation and metallic vapour condensation. CPG is one of the most reliable ignition sources which make possible a reduction of temperature gradient effect and control combustion process. In this paper, different solutions of plasma ignition devices are briefy described. Furthermore, in the paper are presented: idea of our capillary plasma generator, preliminary experimental results (high speed camera pictures) of free air plasma jet propagation and comparison of pictures the impulse effects of plasma and black powder ignition.
Rocznik
Tom
Strony
21--26
Opis fizyczny
Bibliogr. 14 poz., rys.
Twórcy
autor
  • Institute of Armament Technology, Faculty of Mechatronics and Aerospace
  • Institute of Armament Technology, Faculty of Mechatronics and Aerospace
  • Institute of Armament Technology, Faculty of Mechatronics and Aerospace
autor
  • Institute of Optoelectronics, Military University of Technology, 2 Sylwestra Kaliskiego Street, 00-908 Warsaw, PL
autor
  • Institute of Armament Technology, Faculty of Mechatronics and Aerospace
Bibliografia
  • [1] Taylor M.J., Plasma Propellant Interactions in an Electrothermal-Chemical Gun. PhD Thesis, Cranfeld University, Royal Military College of Science, September 2002.
  • [2] Dyvik J., Herbig J., Appleton R., O’Reilly J., Shin J., Recent Activities in Electro-Thermal Chemical Launcher Technologies at BAE Systems. Proceedings of 13th International Symposium on Electromagnetic Launch Technology, May 22-25.2006, Potsdam, Germany 2006.
  • [3] Leciejewski Z.K., Cudziło St., Trends in Development of Propellants in Aspects of Requirements of Future Gun Propellant System. (in Polish) ed. IPO, Materiały Wysokoenergetyczne. vol. 3, (2011), 69-71.
  • [4] Corner J., Theory of the Interior Ballistics of Guns; ed. John Wiley & Sons, Inc. New York. 1950.
  • [5] Sieriebriakow M., Internal Ballistics. (in Polish) ed. MON, Warsaw 1955.
  • [6] STANAG 4115 Land (Edition 2)/1997 Defnition and Determination of Ballistic Properties of Gun Propellants.
  • [7] MIL-STD 286 B, Propellants, Solid: Sampling, Examination and Testing.
  • [8] Smoleński D., Burning of explosives. (in Polish) ed. MON, Warsaw 1979.
  • [9] Baer P.G., Practical Interior Ballistic Analysis of Guns, pp.37-66 in “Progress in Astronautics and Aeronautics. Volume 66 - Interior Ballistics of Guns.” H. Krier and M. Summerfeld ed. American Institute of Aeronautics and Astronautics, Washington, 1979.
  • [10] Beyer R.A., Pesce-Rodriguez R.A., The Response of Propellants to Plasma Radiation IEEE Transactions on Magnetics. vol. 41 No.1 January 2005.
  • [11] Grune D., Hensel D., Combustion Behavior of LOVA-Solid-Propellant by Ignition with Hot Plasma Gases and its Infuence on the Interior Ballistic Cycle; Proceedings of 17th International Symposium on Ballistics, 359-366, Midrand, South Africa 1998.
  • [12] Chen L., Relationship Between Discharge parameters of Capillary and Combustion Behavior of Propellant; Proceedings of 18th International Symposium on Ballistics. 215-219, San Antonio, USA 1999.
  • [13] Lombard J.M., Baschung B., Grune D., Carriere A., Andre P., Analysis of ETC or Classical Manometric Closed Vessel Tests with Coupling of Thermodynamic Equilibrum Calculations Combustion Rate, Energy Losses; Proceedings of 19th International Symposium on Ballistics. 171-178, Interlaken, Switzerland 2000.
  • [14] Taylor M.J., Woodley C.R., Variation in Enhanced Gas Generation Rates in Electrothermal-Chemical Closed Chamber Studies; Proceedings of 19th International Symposium on Ballistics.179-185, Interlaken, Switzerland 2000.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-4178edc3-5d04-43b5-8400-e88601c2fff8
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.