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

You are here: Homepage > Search

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

Panwar, Mardav / Gorrepati, Srinivasa Rao / Chauhan, Manish Kumar

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.

Access

Check access

Check availability in my library

Order at Subito €

Export, share and cite

Document information

Title :

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

Additional title:

Lect.Notes Mechanical Engineering

Contributors:

Singh, Sanjay (editor) / Ramulu, Perumalla Janaki (editor) / Gautam, Sachin Singh (editor) / Panwar, Mardav (author) / Gorrepati, Srinivasa Rao (author) / Chauhan, Manish Kumar (author)

Conference:

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

Published in:

Recent Advances in Aerospace Engineering ; Chapter : 14 ; 181-190

Lecture Notes in Mechanical Engineering

Publication date :

2024-04-28

Size :

10 pages

ISBN :

978-981-97-1306-6 , 978-981-97-1305-9

ISSN :