Design and Analysis of Rocket Model

Abstract: Our project consists of designing and analysing a model rocket with the payload of 10 Kilogram capable of reaching 30kms apogee. It makes a lucid way for students to gain a better experience with the model rocket. In this project "Dhruva M 33" is taken as a fundamental rocket design, and all the factors affecting the model are analysed after designing the rocket which helps students to get a relevant idea about payload model rocket. All the different stages are also mentioned in the project which are primary requirement for the Model rocket. And with the help of stimulation entire process is explained properly. As a result, maximum apogee reached was 33.116 km and ground hit velocity was 49.3 m/s