Development of solid rocket propulsion system at UTM

Rockets have been used from as early as the thirteenth century as fireworks and weapons. However, since then the usage of rockets have been diversified. Nowadays, rockets are used from as small as model rocketry for hobbyist to as large as a satellite launcher. Another diversified usages of rockets...

Full description

Saved in:
Bibliographic Details
Main Authors: Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin, Dahalan, Md. Nizam
Format: Article
Language:en
Published: Faculty of Mechanical Engineering, Universiti Teknologi Malaysia 2004
Subjects:
Online Access:http://eprints.utm.my/6786/1/MohammadNazriMohd2004_Development_of_solid_rocket_propulsion_system.pdf
http://eprints.utm.my/6786/
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1845471690100834304
author Mohd. Jaafar, Mohammad Nazri
Wan Ali, Wan Khairuddin
Dahalan, Md. Nizam
author_facet Mohd. Jaafar, Mohammad Nazri
Wan Ali, Wan Khairuddin
Dahalan, Md. Nizam
author_sort Mohd. Jaafar, Mohammad Nazri
building UTM Library
collection Institutional Repository
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
continent Asia
country Malaysia
description Rockets have been used from as early as the thirteenth century as fireworks and weapons. However, since then the usage of rockets have been diversified. Nowadays, rockets are used from as small as model rocketry for hobbyist to as large as a satellite launcher. Another diversified usages of rockets is as a launch vehicle for cloud seeding. In line with this, over the past decade Universiti Teknologi Malaysia (UTM) has been developing capabilities to launch a small rocket. Due to the low cost of raw materials and ease of production process, composite propellant is the best choice for this purpose. Potassium nitrate based solid propellant has been investigated in order to study their properties and performance. As a result, it is found that this propellant is capable of reaching the necessary range for cloud seeding (6 km - 7 km).
format Article
id my.utm.eprints-6786
institution Universiti Teknologi Malaysia
language en
publishDate 2004
publisher Faculty of Mechanical Engineering, Universiti Teknologi Malaysia
record_format eprints
spelling my.utm.eprints-67862017-05-30T06:49:35Z http://eprints.utm.my/6786/ Development of solid rocket propulsion system at UTM Mohd. Jaafar, Mohammad Nazri Wan Ali, Wan Khairuddin Dahalan, Md. Nizam TJ Mechanical engineering and machinery Rockets have been used from as early as the thirteenth century as fireworks and weapons. However, since then the usage of rockets have been diversified. Nowadays, rockets are used from as small as model rocketry for hobbyist to as large as a satellite launcher. Another diversified usages of rockets is as a launch vehicle for cloud seeding. In line with this, over the past decade Universiti Teknologi Malaysia (UTM) has been developing capabilities to launch a small rocket. Due to the low cost of raw materials and ease of production process, composite propellant is the best choice for this purpose. Potassium nitrate based solid propellant has been investigated in order to study their properties and performance. As a result, it is found that this propellant is capable of reaching the necessary range for cloud seeding (6 km - 7 km). Faculty of Mechanical Engineering, Universiti Teknologi Malaysia 2004-12 Article PeerReviewed application/pdf en http://eprints.utm.my/6786/1/MohammadNazriMohd2004_Development_of_solid_rocket_propulsion_system.pdf Mohd. Jaafar, Mohammad Nazri and Wan Ali, Wan Khairuddin and Dahalan, Md. Nizam (2004) Development of solid rocket propulsion system at UTM. Jurnal Mekanikal, 18 . pp. 111-121. ISSN 0127-3396
spellingShingle TJ Mechanical engineering and machinery
Mohd. Jaafar, Mohammad Nazri
Wan Ali, Wan Khairuddin
Dahalan, Md. Nizam
Development of solid rocket propulsion system at UTM
title Development of solid rocket propulsion system at UTM
title_full Development of solid rocket propulsion system at UTM
title_fullStr Development of solid rocket propulsion system at UTM
title_full_unstemmed Development of solid rocket propulsion system at UTM
title_short Development of solid rocket propulsion system at UTM
title_sort development of solid rocket propulsion system at utm
topic TJ Mechanical engineering and machinery
url http://eprints.utm.my/6786/1/MohammadNazriMohd2004_Development_of_solid_rocket_propulsion_system.pdf
http://eprints.utm.my/6786/
url_provider http://eprints.utm.my/