• DocumentCode
    3188094
  • Title

    ETC Ignition Research on 120 mm Gun in Korea

  • Author

    Kim, Seong Ho ; Yang, Kyung Seung ; Lee, Young Hyun ; Kim, Jin Sung ; Lee, Byung Ha

  • Author_Institution
    Agency for Defense Dev., Daejeon
  • fYear
    2008
  • fDate
    10-13 June 2008
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    An electrothermal-chemical (ETC) propulsion with the control of a combustion process yet requires large electrical energies for an appreciable effect. Referring to the changed tendency of focusing ETC researches on the early ignition phase, ADD (Agency for Defense Development), Korea has been studying an electrothermal ignition for a 120 mm gun using a capillary plasma injector. Under the condition of a limited capillary geometry, design efforts with various liner materials have been done to achieve robust capillary discharges capable of transferring energies around 100 kJ. Electrical properties were estimated with the help of plasma theories and compared with experimental results. Experiments using a closed vessel and a gun chamber simulator have been done to investigate the burning behaviors and the early phase of an electrothermal ignition, respectively. The closed vessel was designed for both a plasma and a conventional ignition. The burning rates could be obtained up to 70 MPa. The gun chamber simulator was designed in the shape of the chamber of a 120 mm gun except for an acrylic chamber wall withstanding up to 30 MPa. Through prior tests using the closed vessel and the gun chamber simulator appropriate electrical energies and propellant have been selected. Firings of the full-scale 120 mm gun have been done using JA2 propellant. Electrical pulses of 1 - 2.5 ms duration in the energy from 20 kJ to 120 kJ were applied. Besides an ignition capability, the results showed a possibility of a control on the peak pressure. Currently, ADD, Korea continues the research to enhance the efficiency of the plasma injector, to compact the pulse forming network, and to investigate the electrothermal ignition properties of LOVA propellant.
  • Keywords
    combustion; electrothermal launchers; plasma applications; weapons; LOVA propellant; capillary plasma injector; combustion process; electrothermal-chemical ignition; electrothermal-chemical propulsion; energy 20 kJ to 120 kJ; gun chamber simulator; liner material; robust capillary discharge; size 120 mm; Combustion; Electrothermal effects; Electrothermal launching; Geometry; Ignition; Phase change materials; Plasma materials processing; Plasma properties; Plasma simulation; Propulsion;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electromagnetic Launch Technology, 2008 14th Symposium on
  • Conference_Location
    Victoria, BC
  • Print_ISBN
    978-1-4244-1832-9
  • Electronic_ISBN
    978-1-4244-1833-6
  • Type

    conf

  • DOI
    10.1109/ELT.2008.37
  • Filename
    4657597