Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Simulation-Based Feasible Robust Design Approach for Multi-Stage Space Launch Vehicle


    Beteiligte:
    Akhtar, Saqlain (Autor:in) / Linshu, He (Autor:in) / Akhtar, Vaqar (Autor:in)

    Kongress:

    46th AIAA Aerospace Sciences Meeting and Exhibit



    Erscheinungsdatum :

    01.01.2008




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Simulation-Based Feasible Robust Design Approach for Multi-Stage Space Launch Vehicle

    Akhtar, S. / Linshu, H. / Akhtar, V. et al. | British Library Conference Proceedings | 2008


    An Efficient Evolutionary Multi-Objective Approach for Robust Design of Multi-Stage Space Launch Vehicle

    Akhtar, S. / Linshu, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006



    Hybrid search multi-discipline feasible design optimization of a typical Space Launch Vehicle

    Bataleblu, Ali Asghar / Roshanian, Jafar / Ebrahimi, Masoud | IEEE | 2015


    Capturing the Global Feasible Design Space for Launch Vehicle Ascent Trajectories

    Steffens, Michael J. / Mavris, Dimitri N. / Edwards, Stephen J. | AIAA | 2015