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Advances in aluminum powder usage as an energetic material and applications for rocket propellant

Energetic materials have been widely used for military purposes. Continuous research programs are performing in the world for the development of the new materials with higher and improved performance comparing with the available ones in order to fulfill the needs of the military in future. Different...

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Main Authors: Sadeghipour, Sakineh, Ghaderian, Javad, A. Wahid, Mazlan
Format: Article
Published: 2012
Subjects:
TP Chemical technology
Online Access:http://eprints.utm.my/id/eprint/46565/
http://dx.doi.org/10.1063/1.4704207
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spelling my.utm.465652017-09-13T09:05:45Z http://eprints.utm.my/id/eprint/46565/ Advances in aluminum powder usage as an energetic material and applications for rocket propellant Sadeghipour, Sakineh Ghaderian, Javad A. Wahid, Mazlan TP Chemical technology Energetic materials have been widely used for military purposes. Continuous research programs are performing in the world for the development of the new materials with higher and improved performance comparing with the available ones in order to fulfill the needs of the military in future. Different sizes of aluminum powders are employed to produce composite rocket propellants with the bases of Ammonium Perchlorate (AP) and Hydroxyl-Terminated-Polybutadiene (HTPB) as oxidizer and binder respectively. This paper concentrates on recent advances in using aluminum as an energetic material and the properties and characteristics pertaining to its combustion. Nano-sized aluminum as one of the most attractable particles in propellants is discussed particularly. 2012 Article PeerReviewed Sadeghipour, Sakineh and Ghaderian, Javad and A. Wahid, Mazlan (2012) Advances in aluminum powder usage as an energetic material and applications for rocket propellant. 4th International Meeting Of Advances In Thermofluids (Imat 2011), Pt 1 And 2, 1440 . ISSN 0094-243X http://dx.doi.org/10.1063/1.4704207
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 TP Chemical technology
spellingShingle TP Chemical technology
Sadeghipour, Sakineh
Ghaderian, Javad
A. Wahid, Mazlan
Advances in aluminum powder usage as an energetic material and applications for rocket propellant
description Energetic materials have been widely used for military purposes. Continuous research programs are performing in the world for the development of the new materials with higher and improved performance comparing with the available ones in order to fulfill the needs of the military in future. Different sizes of aluminum powders are employed to produce composite rocket propellants with the bases of Ammonium Perchlorate (AP) and Hydroxyl-Terminated-Polybutadiene (HTPB) as oxidizer and binder respectively. This paper concentrates on recent advances in using aluminum as an energetic material and the properties and characteristics pertaining to its combustion. Nano-sized aluminum as one of the most attractable particles in propellants is discussed particularly.
format Article
author Sadeghipour, Sakineh
Ghaderian, Javad
A. Wahid, Mazlan
author_facet Sadeghipour, Sakineh
Ghaderian, Javad
A. Wahid, Mazlan
author_sort Sadeghipour, Sakineh
title Advances in aluminum powder usage as an energetic material and applications for rocket propellant
title_short Advances in aluminum powder usage as an energetic material and applications for rocket propellant
title_full Advances in aluminum powder usage as an energetic material and applications for rocket propellant
title_fullStr Advances in aluminum powder usage as an energetic material and applications for rocket propellant
title_full_unstemmed Advances in aluminum powder usage as an energetic material and applications for rocket propellant
title_sort advances in aluminum powder usage as an energetic material and applications for rocket propellant
publishDate 2012
url http://eprints.utm.my/id/eprint/46565/
http://dx.doi.org/10.1063/1.4704207
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score 13.18916

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