• DocumentCode
    1617528
  • Title

    On the simulation of the Space Shuttle main engine

  • Author

    De Abreu-Garcia, J.A. ; Mohammad, A. ; Hartley, T.T.

  • Author_Institution
    Dept. of Electr. Eng., Akron Univ., OH, USA
  • fYear
    1990
  • Firstpage
    188
  • Abstract
    The Space Shuttle main engine simulation is analyzed to determine the means to obtain a faster running simulation. In particular, the valve dynamics module is simulated using three different techniques: Euler´s method, Adams-Bashforth two-step method, and the matrix stability region placement two-step method. It is shown that, by choosing the integration method appropriately, a speed-up factor of about five can be achieved. The valve dynamics module simulation results are then used to make recommendations about the simulation of the Space Shuttle main engine
  • Keywords
    aerospace computing; aerospace engines; aerospace simulation; digital simulation; rockets; space vehicles; Adams-Bashforth two-step method; Euler´s method; Space Shuttle main engine simulation; integration method; matrix stability region placement two-step method; valve dynamics module; Analytical models; Computational modeling; Engines; Nonlinear dynamical systems; Real time systems; Reduced order systems; Rockets; Space shuttles; Stability; Valves;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Industrial Electronics Society, 1990. IECON '90., 16th Annual Conference of IEEE
  • Conference_Location
    Pacific Grove, CA
  • Print_ISBN
    0-87942-600-4
  • Type

    conf

  • DOI
    10.1109/IECON.1990.149135
  • Filename
    149135