The purpose of this paper is to present some aspects regarding the computational model and performance evaluation for three stages launch vehicle (LV) used to inject into circular orbit a small size payload. The computational model consists in numerical simulation of LV evolution for imposed start conditions and optimisation of flight parameter in order to obtain injection into circular orbit. The launcher model presented will be with three degrees of freedom (3DOF) and variable mass. The results analysed will be the flight parameters and the ballistic performances. The discussions area will focus around the technical possibility to evaluate the performance of a small multi-stage launcher using the developed model. From a technical point of view, the paper is focused on ESA project “Study – concept, to achieve a Small Orbital Launcher through zonal cooperation SOL finalised in 2015


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Small Orbital Launcher, Performance Evaluation



    Erschienen in:

    Erscheinungsdatum :

    2016-06-22


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Mathematical Model and Performance Evaluation for a Small Orbital Launcher

    Chelaru, Teodor Viorel ;Chelaru, Adrian | Trans Tech Publications | 2015


    Mathematical Model and Performance Evaluation for a Small Orbital Launcher

    Chelaru, T. V. / Chelaru, A. | British Library Conference Proceedings | 2015


    MOBILE ORBITAL LAUNCHER

    RAVICHANDRAN SRINATH | Europäisches Patentamt | 2023

    Freier Zugriff

    MOBILE ORBITAL LAUNCHER

    RAVICHANDRAN SRINATH | Europäisches Patentamt | 2023

    Freier Zugriff

    MOBILE ORBITAL LAUNCHER

    RAVICHANDRAN SRINATH | Europäisches Patentamt | 2024

    Freier Zugriff