Design and Analysis of First Stage Rocket Engine using Butane and Liquid Oxygen

Volume 9 Issue 3 May - July 2019

Research Paper

Design and Analysis of First Stage Rocket Engine using Butane and Liquid Oxygen

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Department of Mechanical Engineering, Institute of Engineering and Management, Kolkata, West Bengal, India.

Majumder, S. D. (2019). Design and Analysis of First Stage Rocket Engine using Butane and Liquid Oxygen. i-manager’s Journal on Mechanical Engineering, 9(3), 32-41. https://doi.org/10.26634/jme.9.3.15806

Abstract

The manuscript demonstrates the designing of a first stage rocket engine using butane as a fuel and liquid oxygen as the oxidizer combination for yielding higher values of heat of combustion, Mach number, specific Impulse and the exit velocity through the nozzle. The purpose of this research is to provide a fuel oxidizer combination whose heat of combustion would be much higher. With a higher calorific value of butane, it needs very little oxidizer to burn resulting in reducing the weight of the rocket. Chemical Experimental Analysis has shown that the calorific value of butane and liquid oxygen together will yield much higher values in comparison to that of the present combination of fuel and oxidizers. The research paper analyses the design calculations of the space shuttle engine; Solid Works Design of complete Rocket Engine; comparative study of the model rocket with the Orion test rocket; CFD analysis of Rocket Engine.