• Akash Sharma

The design for single stage sounding rocket have been proposed. Modern techniques and methods has been used to optimise the performance of rocket with less weight. The structure of rocket have been designed on the basis of earlier works and theories that were produced by the immense analysis and experiments by different organisations. The aim of the paper is to develop a single stage sounding rocket with overall length constrained less than 1 meter. The structure of rocket have been designed by applying certain constraints such as the payload mass is less than 1000 g and the haack series design is used for the nose cone section for optimum performance. The analysis of different types of fins including clipped fin, trapezoidal fin, tapered fin have been studied rigorously.

ANALYSIS OF DIFFERENT FINS STRUCTURE AND CONCEPTUAL DESIGN OF SINGLE STAGE SOUNDING ROCKET

"ANALYSIS OF DIFFERENT FINS STRUCTURE AND CONCEPTUAL DESIGN OF SINGLE STAGE SOUNDING ROCKET", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 10, page no.b690-b695, October-2021, Available :http://www.jetir.org/papers/JETIR2110175.pdf

"ANALYSIS OF DIFFERENT FINS STRUCTURE AND CONCEPTUAL DESIGN OF SINGLE STAGE SOUNDING ROCKET", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 10, page no. ppb690-b695, October-2021, Available at : http://www.jetir.org/papers/JETIR2110175.pdf