• DocumentCode
    3619764
  • Title

    Passive flow rate control of the fuel and the oxidizer in liquid fuelled rocket motors

  • Author

    B. Yazici;D.E. Gunduz;G. Puskulcu;C. Yildirim;B. Sumer;F.E. Orhan;L.O. Gonc;M.A. Ak

  • Author_Institution
    TUBITAK SAGE, TUBITAK Defence Ind. Res. & Dev. Inst., Ankara, Turkey
  • fYear
    2005
  • fDate
    6/27/1905 12:00:00 AM
  • Firstpage
    315
  • Lastpage
    318
  • Abstract
    For passive flow rate control of oxidizer and fuel of a liquid propellant engine a cavitating venturi is designed, produced and tested.
  • Keywords
    "Fuels","Rockets","Testing","Control systems","Equations","Engines","Valves","Propulsion","Solenoids","Pressure control"
  • Publisher
    ieee
  • Conference_Titel
    Recent Advances in Space Technologies, 2005. RAST 2005. Proceedings of 2nd International Conference on
  • Print_ISBN
    0-7803-8977-8
  • Type

    conf

  • DOI
    10.1109/RAST.2005.1512583
  • Filename
    1512583
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3619764