A design optimization approach of a solid propellant rocket motor is considered. A genetic algorithm (GA) optimization method has been used. The optimized solid rocket motor (SRM) is intended to use as a booster of a flight vehicle, and delivering a specific payload following a predefined prescribed trajectory. Sensitivity analysis of the optimized solution has been conducted using Monte Carlo method to evaluate the effect of uncertainties in design parameters. The results show that the proposed optimization approach was able to find the convergence of the optimal solution with highly acceptable value for conceptual design phase.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Solid Rocket Motor Design Optimization Using Genetic Algorithm



    Erschienen in:

    Erscheinungsdatum :

    2014-04-28


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Solid Rocket Motor Design Using Hybrid Optimization

    Kevin Albarado / Roy Hartfield / Wade Hurston et al. | DOAJ | 2012

    Freier Zugriff

    Solid Rocket Motor Optimization

    Kamm, Yair / Gany, Alon | AIAA | 2008


    Design Optimization of Solid Propellant Rocket Motor

    Konecny, P. / Hruby, V. / Krizan, Z. | British Library Conference Proceedings | 2007


    Design Optimization of Solid Propellant Rocket Motor

    Konecny, P. / Hruby, V. / Krizan, Z. | British Library Conference Proceedings | 2007


    Optimizing a Solid Rocket Motor Boosted Ramjet Powered Missile Using a Genetic Algorithm

    Hartfield, Roy / Jenkins, Rhonald / Burkhalter, John | AIAA | 2005