Effect of oxidizer-fuel mixture ratio to the pressure exponent of ammonium perchlorate based composite propellant
In this paper, experimental investigation of pressure exponent in burning rate of composite propellant was conducted. Four sets of different propellant compositions had been prepared with the combination of Ammonium Perchlorate (AP) as an oxidizer, Aluminum (Al) as fuel and Hydroxy-Terminated Polybu...
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| Main Authors: | , |
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| Format: | Article |
| Published: |
2012
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| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/46863/ http://dx.doi.org/10.4028/www.scientific.net/AMM.110-116.1380 |
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| Institution: | Universiti Teknologi Malaysia |