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INTERNATIONAL JOURNAL OF NOVEL RESEARCH AND DEVELOPMENT International Peer Reviewed & Refereed Journals, Open Access Journal ISSN Approved Journal No: 2456-4184 | Impact factor: 8.76 | ESTD Year: 2016 Scholarly open access journals, Peer-reviewed, and Refereed Journals, Impact factor 8.76 (Calculate by google scholar and Semantic Scholar | AI-Powered Research Tool) , Multidisciplinary, Monthly, Indexing in all major database & Metadata, Citation Generator, Digital Object Identifier(DOI) |
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| Paper Title: | Solid Rocket motor for academics uses |
| Authors Name: | Naman Bajpai |
| Download E-Certificate: | Download |
| Author Reg. ID: |
IJNRD_183288
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| Published Paper Id: | IJNRD2210028 |
| Published In: | Volume 7 Issue 10, October-2022 |
| DOI: | |
| Abstract: | The invention of experimental sounding rockets has considerably improved the area of aeronautical engineering. However, experimental sounding rockets are rarely used for student research projects in Indian colleges. The scarcity of rocket motors is a significant impediment to deploying sounding rockets in research efforts. When developing sounding rockets for research and instructional purposes, we encountered this challenge due to sophisticated machining and explosive propellants. The major goal of this study is to design and build solid rocket engines that will be used to power experimental sounding rockets. An initial review focuses on the fundamental design, examining various approaches to propellant composition. Propeller availability, simplicity of production, and casting efficiency are all significant factors to consider while determining the best propellant deployment. Theoretical values are generated for combustion chamber parameters. These data are used to create theoretical values for combustion chamber characteristics, and materials are chosen appropriately. A fundamental small-scale experimental design is developed and thoroughly tested. After all test and theoretical data have been incorporated, the final engine will be constructed and tested against the predicted power output of her two propellants, RNX and Candy Fuel. This document is a fantastic resource for students concerned with rocket testing since it outlines all of the pieces required to construct a rocket motor with a specific impulse of interest. Engine structures are utilized in educational sounding rockets for atmospheric and aerodynamic study. This engine is a low-cost propulsion system that may be utilized for research in domains other than aerospace. |
| Keywords: | Rockets,Aerospace,Solid propulsion |
| Cite Article: | "Solid Rocket motor for academics uses", International Journal of Novel Research and Development (www.ijnrd.org), ISSN:2456-4184, Vol.7, Issue 10, page no.215-222, October-2022, Available :http://www.ijnrd.org/papers/IJNRD2210028.pdf |
| Downloads: | 000118750 |
| ISSN: |
2456-4184 | IMPACT FACTOR: 8.76 Calculated By Google Scholar| ESTD YEAR: 2016 An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 8.76 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator |
| Publication Details: |
Published Paper ID:IJNRD2210028 Registration ID: 183288 Published In: Volume 7 Issue 10, October-2022 DOI (Digital Object Identifier): Page No: 215-222 Country: Mumbai, Maharashtra, India Research Area: Engineering Publisher : IJ Publication Published Paper URL : https://www.ijnrd.org/viewpaperforall?paper=IJNRD2210028 Published Paper PDF: https://www.ijnrd.org/papers/IJNRD2210028 |
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ISSN: 2456-4184
Impact Factor: 8.76 and ISSN APPROVED
Journal Starting Year (ESTD) : 2016
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