期刊名称：International Journal of Advances in Engineering and Management
电子版ISSN：2395-5252
出版年度：2021
卷号：3
期号：11
页码：612-617
DOI：10.35629/5252-0311381409
语种：English
出版社：IJAEM JOURNAL
摘要：The model rocket was designed to reach the apogee of 30000m carrying apayload of 10kg. So, it was designed with 3 stages (2 booster stages and 1 sustainer stage). This model is designed such that, the total weight of the rocket is 148.211 kg and it is reaching an apogee of 33.173 km. 1st stage consists of the nose cone, body tube and fins. 2nd and 3rd stage consists of just the body tube and the fins. To connect each of the body tubes the coupler has been installed. While analyzing the flight simulation for our Model Rocket, the Altitude and Vertical velocity is plotted with respect to time and Different stages of flight are shown in the simulation graph. For example, Motor burnout, stage separation etc. here launch rod length was set to 1100 cm (double the length of the rocket).
