In this study, a mission design process for space launch vehicles was established based on the systems engineering process and implemented to obtain the system baseline and the mission profiles. The process was sophisticatedly developed for users to make necessary decisions and to obtain design results rapidly. Database for the world's competitive rocket systems was built for the use of data mining. Seven disciplinary modules, such as the Weight Estimation, Mission Velocity, Staging, Propulsion, Configuration, Aerodynamics, and Trajectory, were developed for low fidelity analysis, and integrated as a system level process. In addition, several data mining techniques were adapted to the process as an alternative method of the requirements analysis, and utilized to provide the initial values of design parameters. Based on the established process, a design was optimized, and it was successfully converged. Through the multidisciplinary design optimization, it was possible to obtain the system baseline and the trajectory.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Multidisciplinary mission design optimization for space launch vehicles based on sequential design process




    Erscheinungsdatum :

    2016




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik
    Lokalklassifikation TIB:    275/7040



    Multidisciplinary mission design optimization for space launch vehicles based on sequential design process

    Shu, Jung-Il / Kim, Jin-Wook / Lee, Jae-Woo et al. | SAGE Publications | 2016


    Multidisciplinary Design Optimization to Reusable Space Launch Vehicles

    Tsuchiya, T. / Mori, T. / Taguchi, H. et al. | British Library Conference Proceedings | 2002


    Multidisciplinary design tool for system and mission optimization of launch vehicles

    Rahn, M. / Schoettle, U. / Messerschmid, E. | AIAA | 1996


    Multidisciplinary Design Tool for System and Mission Optimization of Launch Vehicles

    Rahn, M. / Schottle, U. / Messerschmid, E. et al. | British Library Conference Proceedings | 1996


    MULTIDISCIPLINARY DESIGN OPTIMIZATION OF REUSABLE LAUNCH VEHICLES

    Cusick, Andrew / Kontis, Konstantinos / Nikbay, Melike | TIBKAT | 2020