Now showing items 1-2 of 2

  • Design and implementation of a second stage nozzle for a low cost mini-launcher 

    Arias Novo, Ernest (Universitat Politècnica de Catalunya, 2011-03-31)
    Master thesis (pre-Bologna period)
    Open Access
    This study is addressed to design and build a nozzle for a second stage of a solid propellant APCP (Ammonium Perchlorate Composite Propellant) based as a part of an EETAC grand. We will use the simulator Moon2.0 to design ...
  • Study of minimum length, supersonic nozzle design using the Method of Characteristics 

    Murnaghan Murnaghan, Murrough (Universitat Politècnica de Catalunya, 2019-06)
    Master thesis
    Open Access
    This report outlines the pertinent theory and methods for supersonic nozzle design using the method of characteristics. The programmes developed design ideal nozzle contours, using numerical methods based on the gas ...