Please use this identifier to cite or link to this item:
https://elibrary.tucl.edu.np/handle/123456789/17744
Title: | Design, Build and Test Small Scale Liquid Rocket Engine |
Authors: | Mishra, Krishna Kant Gautam, Prajwal Yadav, Prakash |
Keywords: | Design,;Build,;Rocket |
Issue Date: | Mar-2023 |
Publisher: | I.O.E. Pulchowk Campus |
Institute Name: | Institute of Engineering |
Level: | Bachelor |
Abstract: | The project entitled, “Design, Build and Test Small Scale Liquid Rocket Engine” reports about the liquid rocket engine which is a device in which liquid propellant is used to produce thrust. In this project at least 200N of thrust is aimed to be generated. This project aims to generate thrust by using liquid propellant which is the combination of oxidizer and fuel. This project is an experimental study of the amount of thrust produced by the liquid rocket engine and design of various components needed to achieve the project target. The combustion chamber, nozzle, cylinder and fuel selection and design are focused and thus the target of the project is being achieved. This project helps us implement our knowledge and understanding of propulsion system and make us practically study its behavior which will surely be helpful for enhancing our knowledge and understanding of the propulsion phenomenon. |
Description: | The project entitled, “Design, Build and Test Small Scale Liquid Rocket Engine” reports about the liquid rocket engine which is a device in which liquid propellant is used to produce thrust. In this project at least 200N of thrust is aimed to be generated. |
URI: | https://elibrary.tucl.edu.np/handle/123456789/17744 |
Appears in Collections: | Mechanical and Aerospace Engineering |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Krishna Kant et al. project report mechanical nd aerospace.pdf | 2.53 MB | Adobe PDF | View/Open |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.