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Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant

The development of rocket motor using potassium nitrate, carbon and sulphur mixture has successfully been developed by researchers and students from UTM and recently a new combination for solid propellant is being created. The new solid propellant will combine a composition of Ammonium perchlorate,...

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Main Authors: Ab Wahid, Mastura, Wan Ali, Wan Khairuddin
Format: Conference or Workshop Item
Published: 2009
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://eprints.utm.my/id/eprint/15034/
https://dx.doi.org/10.1063/1.3464841
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spelling my.utm.150342020-07-20T01:23:53Z http://eprints.utm.my/id/eprint/15034/ Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant Ab Wahid, Mastura Wan Ali, Wan Khairuddin TJ Mechanical engineering and machinery The development of rocket motor using potassium nitrate, carbon and sulphur mixture has successfully been developed by researchers and students from UTM and recently a new combination for solid propellant is being created. The new solid propellant will combine a composition of Ammonium perchlorate, NH4ClO4 with aluminium, Al and Hydroxyl Terminated Polybutadiene, HTPB as the binder. It is the aim of this research to design and fabricate a new rocket motor that will produce a thrust of 200N by using this new solid propellant. A static test is done to obtain the thrust produced by the rocket motor and analyses by observation and also calculation will be done. The experiment for the rocket motor is successful but the thrust did not achieve its required thrust. 2009 Conference or Workshop Item PeerReviewed Ab Wahid, Mastura and Wan Ali, Wan Khairuddin (2009) Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant. In: The 2nd International Meeting on Advances in Thermo-Fluids (IMAT) 2009, 2009, Taman Safari, Bogor, Indonesia. https://dx.doi.org/10.1063/1.3464841
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Ab Wahid, Mastura
Wan Ali, Wan Khairuddin
Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
description The development of rocket motor using potassium nitrate, carbon and sulphur mixture has successfully been developed by researchers and students from UTM and recently a new combination for solid propellant is being created. The new solid propellant will combine a composition of Ammonium perchlorate, NH4ClO4 with aluminium, Al and Hydroxyl Terminated Polybutadiene, HTPB as the binder. It is the aim of this research to design and fabricate a new rocket motor that will produce a thrust of 200N by using this new solid propellant. A static test is done to obtain the thrust produced by the rocket motor and analyses by observation and also calculation will be done. The experiment for the rocket motor is successful but the thrust did not achieve its required thrust.
format Conference or Workshop Item
author Ab Wahid, Mastura
Wan Ali, Wan Khairuddin
author_facet Ab Wahid, Mastura
Wan Ali, Wan Khairuddin
author_sort Ab Wahid, Mastura
title Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
title_short Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
title_full Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
title_fullStr Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
title_full_unstemmed Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
title_sort design and fabrication of a 200n thrust rocket motor based on nh4clo4 + al + htpb as solid propellant
publishDate 2009
url http://eprints.utm.my/id/eprint/15034/
https://dx.doi.org/10.1063/1.3464841
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score 13.209306

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