In the current study, point-mass trajectory simulation model (PM-TSM) has been developed using MATLAB. Parametric studies of an un-guided rocket at user given parameters and launch conditions were performed as a part of system studies for an un-guided rocket. While conducting parametric studies, a total of 39 cases were studied for GRAD, artillery rocket with varying launch conditions. It is found that GRAD performed better than S-13 T un-guided aerial launched rocket system at 1000 and 2000-m launch altitude with launch angle of 10 and 0 degrees, respectively. The range achieved by GRAD was more than 4000 m, which is considered as the maximum range of S-13 T rockets.


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    Titel :

    Parametric Studies of an Un-Guided Rocket Using Simple Point-Mass Trajectory Simulation Model


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Singh, Sanjay (Herausgeber:in) / Ramulu, Perumalla Janaki (Herausgeber:in) / Gautam, Sachin Singh (Herausgeber:in) / Panwar, Mardav (Autor:in) / Gorrepati, Srinivasa Rao (Autor:in) / Chauhan, Manish Kumar (Autor:in)

    Kongress:

    International Conference on Modern Research in Aerospace Engineering ; 2023 ; Noida, India September 21, 2023 - September 22, 2023



    Erscheinungsdatum :

    28.04.2024


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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