Paper Details

CONCEPTUAL DESIGN AND ANALYSIS OF TWO STAGE SOUNDING ROCKET

Vol. 7, Jan-Dec 2021 | Page: 52-72

Ankit Kumar Mishra
Department of Research and Development, Abyom Space tech and Defence Pvt. Ltd, Gorahkpur-274402, India

Kshitij Gandhi
Department of Aerospace Engineering, School of Aeronautics, Rajasthan- 301705, India

Kuldeep Sharma
Department of Aerospace Engineering, Hindustan Institute of Technology and Sciences, Tamil Nadu -521230, India.

Neerumalla Sumanth

Y Krishna Teja

Received: 15-07-2021, Accepted: 22-08-2021, Published Online: 01-09-2021


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Abstract

The objective of this paper is to design a two stage sounding rocket and its nozzles using fusion 360 and analysis of different properties using simulation on ANSYS software. The rocket is designed to reach maximum apogee to perform scientific experiments and can be recovered safely after use. Number of CFD simulations were done on structural design with different parameters to analyze the aerodynamic characteristics of the different stages of rocket and the verification of the nozzles. Wish you find your UK best replica breitling watches online.
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